MPU-9150 [TDK]

IMU (惯性测量设备);
MPU-9150
型号: MPU-9150
厂家: TDK ELECTRONICS    TDK ELECTRONICS
描述:

IMU (惯性测量设备)

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InvenSense Inc.  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
1197 Borregas Ave, Sunnyvale, CA 94089 U.S.A.  
Tel: +1 (408) 988-7339 Fax: +1 (408) 988-8104  
Website: www.invensense.com  
Release Date: 9/18/2013  
MPU-9150  
Product Specification  
Revision 4.3  
Proprietary and Confidential  
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Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
CONTENTS  
1
2
3
REVISION HISTORY ...................................................................................................................................5  
PURPOSE AND SCOPE .............................................................................................................................6  
PRODUCT OVERVIEW...............................................................................................................................7  
3.1  
MPU-9150 OVERVIEW ........................................................................................................................7  
APPLICATIONS...........................................................................................................................................8  
FEATURES..................................................................................................................................................9  
4
5
5.1  
GYROSCOPE FEATURES.......................................................................................................................9  
ACCELEROMETER FEATURES ...............................................................................................................9  
MAGNETOMETER FEATURES.................................................................................................................9  
ADDITIONAL FEATURES ........................................................................................................................9  
MOTIONPROCESSING.........................................................................................................................10  
CLOCKING.........................................................................................................................................10  
5.2  
5.3  
5.4  
5.5  
5.6  
6
ELECTRICAL CHARACTERISTICS.........................................................................................................11  
6.1  
GYROSCOPE SPECIFICATIONS............................................................................................................11  
ACCELEROMETER SPECIFICATIONS.....................................................................................................12  
MAGNETOMETER SPECIFICATIONS......................................................................................................13  
ELECTRICAL AND OTHER COMMON SPECIFICATIONS............................................................................14  
ELECTRICAL SPECIFICATIONS, CONTINUED .........................................................................................15  
ELECTRICAL SPECIFICATIONS, CONTINUED .........................................................................................16  
ELECTRICAL SPECIFICATIONS, CONTINUED .........................................................................................17  
I2C TIMING CHARACTERIZATION..........................................................................................................18  
ABSOLUTE MAXIMUM RATINGS ...........................................................................................................19  
6.2  
6.3  
6.4  
6.5  
6.6  
6.7  
6.8  
6.9  
7
APPLICATIONS INFORMATION..............................................................................................................20  
7.1  
PIN OUT AND SIGNAL DESCRIPTION....................................................................................................20  
TYPICAL OPERATING CIRCUIT.............................................................................................................21  
BILL OF MATERIALS FOR EXTERNAL COMPONENTS..............................................................................21  
RECOMMENDED POWER-ON PROCEDURE ...........................................................................................22  
BLOCK DIAGRAM ...............................................................................................................................23  
OVERVIEW ........................................................................................................................................23  
THREE-AXIS MEMS GYROSCOPE WITH 16-BIT ADCS AND SIGNAL CONDITIONING................................24  
THREE-AXIS MEMS ACCELEROMETER WITH 16-BIT ADCS AND SIGNAL CONDITIONING ........................24  
THREE-AXIS MEMS MAGNETOMETER WITH 13-BIT ADCS AND SIGNAL CONDITIONING .........................24  
7.2  
7.3  
7.4  
7.5  
7.6  
7.7  
7.8  
7.9  
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7.10  
7.11  
7.12  
7.13  
7.14  
7.15  
7.16  
7.17  
7.18  
7.19  
7.20  
7.21  
7.22  
DIGITAL MOTION PROCESSOR ............................................................................................................24  
PRIMARY I2C .....................................................................................................................................24  
AUXILIARY I2C SERIAL INTERFACE ......................................................................................................25  
SELF-TEST........................................................................................................................................25  
MPU-9150 SOLUTION FOR 10-AXIS SENSOR FUSION USING I2C INTERFACE........................................26  
PROCEDURE FOR DIRECTLY ACCESSING THE AK8975 3-AXIS COMPASS .............................................28  
INTERNAL CLOCK GENERATION ..........................................................................................................28  
SENSOR DATA REGISTERS.................................................................................................................29  
FIFO ................................................................................................................................................29  
INTERRUPTS......................................................................................................................................29  
DIGITAL-OUTPUT TEMPERATURE SENSOR ..........................................................................................29  
BIAS AND LDO ..................................................................................................................................30  
CHARGE PUMP ..................................................................................................................................30  
8
9
PROGRAMMABLE INTERRUPTS............................................................................................................31  
DIGITAL INTERFACE ...............................................................................................................................32  
9.1  
I2C SERIAL INTERFACE.......................................................................................................................32  
I2C INTERFACE ..................................................................................................................................32  
I2C COMMUNICATIONS PROTOCOL......................................................................................................32  
I2C TERMS ........................................................................................................................................35  
9.2  
9.3  
9.4  
10 SERIAL INTERFACE CONSIDERATIONS...............................................................................................36  
10.1  
10.2  
10.3  
MPU-9150 SUPPORTED INTERFACES.................................................................................................36  
LOGIC LEVELS ...................................................................................................................................36  
LOGIC LEVELS DIAGRAM ....................................................................................................................37  
11 ASSEMBLY ...............................................................................................................................................38  
11.1  
11.2  
11.3  
11.4  
11.5  
11.6  
11.7  
11.8  
11.9  
11.10  
ORIENTATION OF AXES ......................................................................................................................38  
PACKAGE DIMENSIONS ......................................................................................................................39  
PCB DESIGN GUIDELINES:.................................................................................................................40  
ASSEMBLY PRECAUTIONS ..................................................................................................................41  
REFLOW SPECIFICATION ....................................................................................................................43  
STORAGE SPECIFICATIONS.................................................................................................................44  
PACKAGE MARKING SPECIFICATION....................................................................................................44  
TAPE & REEL SPECIFICATION.............................................................................................................45  
LABEL ...............................................................................................................................................46  
PACKAGING...................................................................................................................................47  
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11.11  
REPRESENTATIVE SHIPPING CARTON LABEL...................................................................................48  
12 RELIABILITY .............................................................................................................................................49  
12.1  
12.2  
QUALIFICATION TEST POLICY .............................................................................................................49  
QUALIFICATION TEST PLAN ................................................................................................................49  
13 ENVIRONMENTAL COMPLIANCE...........................................................................................................50  
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1
Revision History  
Revision  
Date  
Revision Description  
05/27/2011  
06/14/2011  
1.0  
2.0  
Initial Release of Product Specification  
Modified for Rev C Silicon (sections 5.2, 6.2, 6.4, 6.6, 8.2, 8.3, 8.4)  
Edits for clarity (several sections)  
10/21/2011  
2.1  
Updated Supply current vs. operating modes (sections 5.3, 5.4, 6.4)  
Modified Self-Test Response of Accelerometers (section 6.2)  
Modified absolute maximum rating for acceleration (section 6.9)  
Updated latch up current rating (sections 6.9, 12.2)  
Modified package dimensions and PCB design guidelines (sections 11.2, 11.3)  
Updated assembly precautions (section 11.4)  
Updated qualification test plan (section 12.2)  
Edits for clarity (several sections)  
10/24/2011  
3.0  
Modified for Rev D Silicon (sections 6.2, 8.2, 8.3, 8.4)  
Edits for Clarity (several sections)  
12/23/2011  
05/14/2012  
3.1  
4.0  
Updated package dimensions (section 11.2)  
Added Gyroscope specifications (section 6.1)  
Added Accelerometer specifications (section 6.2)  
Updated Electrical Other Common Specifications (section 6.3)  
Updated latch-up information (section 6.9)  
Updated Block Diagram (section 7.5)  
Update Self-Test description (section 7.13)  
Updated PCB design guidelines (section 11.3)  
Updated packing and shipping information (sections 11.8, 11.9, 11.10, 11.11)  
Updated reliability references (section 12.2)  
8/28/2013  
4.1  
Removed “Advanced Information” watermark. Updated section 2.0, 6.5, 6.7,  
1.7, 7.2, 7.15, 8, 10.3 and 11.8. Removed section 8.1.  
9/13/2013  
9/18/2013  
.
4.2  
4.3  
Updated Section 6.  
Updated Section 5.5 & 8.  
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2
Purpose and Scope  
This product specification provides information regarding the electrical specification and design related  
information for the MPU-9150™ Motion Processing Unit™ or MPU™.  
Electrical characteristics are based upon design analysis and simulation results only. Specifications are  
subject to change without notice. For references to register map and descriptions of individual registers,  
please refer to the MPU-9150 Register Map and Register Descriptions document.  
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3
Product Overview  
3.1  
MPU-9150 Overview  
MotionInterface™ is becoming a “must-have” function being adopted by smartphone and tablet  
manufacturers due to the enormous value it adds to the end user experience. In smartphones, it finds use in  
applications such as gesture commands for applications and phone control, enhanced gaming, augmented  
reality, panoramic photo capture and viewing, and pedestrian and vehicle navigation. With its ability to  
precisely and accurately track user motions, MotionTracking technology can convert handsets and tablets  
into powerful 3D intelligent devices that can be used in applications ranging from health and fitness  
monitoring to location-based services. Key requirements for MotionInterface enabled devices are small  
package size, low power consumption, high accuracy and repeatability, high shock tolerance, and application  
specific performance programmability all at a low consumer price point.  
The MPU-9150 is the world’s first integrated 9-axis MotionTracking device that combines a 3-axis MEMS  
gyroscope, a 3-axis MEMS accelerometer, a 3-axis MEMS magnetometer and a Digital Motion Processor™  
(DMP) hardware accelerator engine. The MPU-9150 is an ideal solution for handset and tablet  
applications, game controllers, motion pointer remote controls, and other consumer devices. The MPU-  
9150’s 9-axis MotionFusion combines acceleration and rotational motion plus heading information into a  
single data stream for the application. This MotionProcessingtechnology integration provides a smaller  
footprint and has inherent cost advantages compared to discrete gyroscope, accelerometer, plus  
magnetometer solutions. The MPU-9150 is also designed to interface with multiple non-inertial digital  
sensors, such as pressure sensors, on its auxiliary I2C port to produce a 10-Axis sensor fusion output. The  
MPU-9150 is a 3rd generation motion processor and is footprint compatible with the MPU-60X0 and MPU-  
30X0 families.  
The MPU-9150 features three 16-bit analog-to-digital converters (ADCs) for digitizing the gyroscope outputs,  
three 16-bit ADCs for digitizing the accelerometer outputs and three 13-bit ADCs for digitizing the  
magnetometer outputs. For precision tracking of both fast and slow motions, the parts feature a user-  
programmable gyroscope full-scale range of ±250, ±500, ±1000, and ±2000°/sec (dps), a user-  
programmable accelerometer full-scale range of ±2g, ±4g, ±8g, and ±16g, and a magnetometer full-scale  
range of ±1200µT.  
The MPU-9150 is a multi-chip module (MCM) consisting of two dies integrated into a single LGA package.  
One die houses the 3-Axis gyroscope and the 3-Axis accelerometer. The other die houses the AK8975 3-  
Axis magnetometer from Asahi Kasei Microdevices Corporation.  
An on-chip 1024 Byte FIFO buffer helps lower system power consumption by allowing the system processor  
to read the sensor data in bursts and then enter a low-power mode as the MPU collects more data. With all  
the necessary on-chip processing and sensor components required to support many motion-based use  
cases, the MPU-9150 uniquely supports a variety of advanced motion-based applications entirely on-chip.  
The MPU-9150 thus enables low-power MotionProcessing in portable applications with reduced processing  
requirements for the system processor. By providing an integrated MotionFusion output, the DMP in the  
MPU-9150 offloads the intensive MotionProcessing computation requirements from the system processor,  
minimizing the need for frequent polling of the motion sensor output.  
Communication with all registers of the device is performed using I2C at 400 kHz. Additional features include  
an embedded temperature sensor and an on-chip oscillator with ±1% variation over the operating  
temperature range.  
By leveraging its patented and volume-proven Nasiri-Fabrication platform, which integrates MEMS wafers  
with companion CMOS electronics through wafer-level bonding, InvenSense has driven the MPU-9150  
package size down to a revolutionary footprint of 4x4x1mm (LGA), while providing the highest performance,  
lowest noise, and the lowest cost semiconductor packaging required for handheld consumer electronic  
devices. The part features a robust 10,000g shock tolerance, and has programmable low-pass filters for the  
gyroscopes, accelerometers, magnetometers, and the on-chip temperature sensor.  
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4
Applications  
BlurFree™ technology (for Video/Still Image Stabilization)  
AirSign™ technology (for Security/Authentication)  
TouchAnywhere™ technology (for “no touch” UI Application Control/Navigation)  
MotionCommand™ technology (for Gesture Short-cuts)  
Motion-enabled game and application framework  
InstantGesture™ iG™ gesture recognition  
Location based services, points of interest, and dead reckoning  
Handset and portable gaming  
Motion-based game controllers  
3D remote controls for Internet connected DTVs and set top boxes, 3D mice  
Wearable sensors for health, fitness and sports  
Toys  
Pedestrian based navigation  
Navigation  
Electronic Compass  
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5
Features  
5.1  
Gyroscope Features  
The triple-axis MEMS gyroscope in the MPU-9150 includes a wide range of features:  
Digital-output X-, Y-, and Z-Axis angular rate sensors (gyroscopes) with a user-programmable full-  
scale range of ±250, ±500, ±1000, and ±2000°/sec  
External sync signal connected to the FSYNC pin supports image, video and GPS synchronization  
Integrated 16-bit ADCs enable simultaneous sampling of gyros  
Enhanced bias and sensitivity temperature stability reduces the need for user calibration  
Improved low-frequency noise performance  
Digitally-programmable low-pass filter  
Factory calibrated sensitivity scale factor  
User self-test  
5.2  
Accelerometer Features  
The triple-axis MEMS accelerometer in MPU-9150 includes a wide range of features:  
Digital-output 3-Axis accelerometer with a programmable full scale range of ±2g, ±4g, ±8g and ±16g  
Integrated 16-bit ADCs enable simultaneous sampling of accelerometers while requiring no external  
multiplexer  
Orientation detection and signaling  
Tap detection  
User-programmable interrupts  
High-G interrupt  
User self-test  
5.3  
Magnetometer Features  
The triple-axis MEMS magnetometer in MPU-9150 includes a wide range of features:  
3-axis silicon monolithic Hall-effect magnetic sensor with magnetic concentrator  
Wide dynamic measurement range and high resolution with lower current consumption.  
Output data resolution is 13 bit (0.3 µT per LSB)  
Full scale measurement range is ±1200 µT  
Self-test function with internal magnetic source to confirm magnetic sensor operation on end  
products  
5.4  
Additional Features  
The MPU-9150 includes the following additional features:  
9-Axis MotionFusion via on-chip Digital Motion Processor (DMP)  
Auxiliary master I2C bus for reading data from external sensors (e.g., pressure sensor)  
Flexible VLOGIC reference voltage supports multiple I2C interface voltages  
Smallest and thinnest package for portable devices: 4x4x1mm LGA  
Minimal cross-axis sensitivity between the accelerometer, gyroscope and magnetometer axes  
1024 byte FIFO buffer reduces power consumption by allowing host processor to read the data in  
bursts and then go into a low-power mode as the MPU collects more data  
Digital-output temperature sensor  
User-programmable digital filters for gyroscope, accelerometer, and temp sensor  
10,000 g shock tolerant  
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400kHz Fast Mode I2C for communicating with all registers  
MEMS structure hermetically sealed and bonded at wafer level  
RoHS and Green compliant  
5.5  
MotionProcessing  
Internal Digital Motion Processing™ (DMP™) engine supports 3D MotionProcessing and gesture  
recognition algorithms  
The MPU-9150 collects gyroscope, accelerometer and magnetometer data while synchronizing data  
sampling at a user defined rate. The total dataset obtained by the MPU-9150 includes 3-Axis  
gyroscope data, 3-Axis accelerometer data, 3-Axis magnetometer data, and temperature data.  
The FIFO buffers the complete data set, reducing timing requirements on the system processor by  
allowing the processor burst read the FIFO data. After burst reading the FIFO data, the system  
processor can save power by entering a low-power sleep mode while the MPU collects more data.  
Programmable interrupt supports features such as gesture recognition, panning, zooming, scrolling,  
tap detection, and shake detection  
Digitally-programmable low-pass filters.  
Low-power pedometer functionality allows the host processor to sleep while the DMP maintains the  
step count.  
5.6  
Clocking  
On-chip timing generator ±1% frequency variation over full temperature range  
Optional external clock inputs of 32.768kHz or 19.2MHz  
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6
Electrical Characteristics  
6.1  
Gyroscope Specifications  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
PARAMETER  
CONDITIONS  
MIN  
TYP  
MAX  
UNITS  
NOTES  
GYROSCOPE SENSITIVITY  
Full-Scale Range  
FS_SEL=0  
FS_SEL=1  
FS_SEL=2  
FS_SEL=3  
±250  
±500  
±1000  
±2000  
16  
º/s  
º/s  
º/s  
º/s  
Gyroscope ADC Word Length  
Sensitivity Scale Factor  
bits  
FS_SEL=0  
FS_SEL=1  
FS_SEL=2  
FS_SEL=3  
25°C  
131  
LSB/(º/s)  
LSB/(º/s)  
LSB/(º/s)  
LSB/(º/s)  
%
65.5  
32.8  
16.4  
Sensitivity Scale Factor Tolerance  
-3  
+3  
Sensitivity Scale Factor Variation Over  
Temperature  
-40°C to +85°C  
±0.04  
%/°C  
Nonlinearity  
Best fit straight line; 25°C  
0.2  
±2  
%
%
Cross-Axis Sensitivity  
GYROSCOPE ZERO-RATE OUTPUT (ZRO)  
Initial ZRO Tolerance  
Component level (25°C)  
-40°C to +85°C  
FS_SEL=0  
±20  
±20  
º/s  
º/s  
ZRO Variation Over Temperature  
GYROSCOPE NOISE PERFORMANCE  
Total RMS Noise  
DLPFCFG=2 (92Hz)  
At 10Hz  
0.06  
º/s-rms  
Rate Noise Spectral Density  
0.005  
º/s/Hz  
GYROSCOPE MECHANICAL  
FREQUENCIES  
X-Axis  
30  
27  
24  
33  
30  
27  
36  
33  
30  
kHz  
kHz  
kHz  
Y-Axis  
Z-Axis  
LOW PASS FILTER RESPONSE  
Programmable Range  
5
4
256  
Hz  
Hz  
ms  
OUTPUT DATA RATE  
Programmable  
DLPFCFG=0  
to ±1º/s of Final  
8,000  
GYROSCOPE START-UP TIME  
ZRO Settling  
30  
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6.2  
Accelerometer Specifications  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
PARAMETER  
CONDITIONS  
MIN  
TYP  
MAX  
UNITS  
NOTES  
ACCELEROMETER SENSITIVITY  
Full-Scale Range  
AFS_SEL=0  
±2  
±4  
g
AFS_SEL=1  
g
AFS_SEL=2  
±8  
g
AFS_SEL=3  
±16  
g
ADC Word Length  
Output in two’s complement format  
AFS_SEL=0  
16  
bits  
LSB/g  
LSB/g  
LSB/g  
LSB/g  
%
Sensitivity Scale Factor  
16,384  
8,192  
4,096  
2,048  
±3  
AFS_SEL=1  
AFS_SEL=2  
AFS_SEL=3  
Initial Calibration Tolerance  
Sensitivity Change vs. Temperature  
Nonlinearity  
AFS_SEL=0, -40°C to +85°C  
Best Fit Straight Line  
±0.02  
0.5  
%/°C  
%
ZERO-G OUTPUT  
Initial Calibration Tolerance  
X and Y axes  
Z axis  
±80  
mg  
mg  
±150  
Change over specified temperature –  
Component level -25°C to 85°C  
X & Y Axis  
Z Axis  
±0.75  
±1.50  
mg/°C  
mg/°C  
NOISE PERFORMANCE  
g/Hz  
Power Spectral Density  
X, Y & Z Axes, @10Hz,  
AFS_SEL=0 & ODR=1kHz  
AFS = 0 @100Hz  
400  
4
mg-rms  
Total RMS Noise  
LOW PASS FILTER RESPONSE  
Programmable Range  
Programmable Range  
5
4
260  
Hz  
OUTPUT DATA RATE  
1,000  
Hz  
INTELLIGENCE FUNCTION  
INCREMENT  
32  
mg/LSB  
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6.3  
Magnetometer Specifications  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
The information in the following table is from the AKM AK8975 datasheet.  
PARAMETER  
CONDITIONS  
MIN  
TYP  
MAX  
UNITS  
NOTES  
MAGNETOMETER SENSITIVITY  
Full-Scale Range  
±1200  
13  
µT  
ADC Word Length  
Output in two’s complement format  
bits  
Sensitivity Scale Factor  
ZERO-FIELD OUTPUT  
Initial Calibration Tolerance  
0.285  
-1000  
0.3  
0.315  
1000  
µT /LSB  
LSB  
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6.4  
Electrical and Other Common Specifications  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
PARAMETER  
CONDITIONS  
MIN  
TYP  
MAX  
Units  
Notes  
TEMPERATURE SENSOR  
Range  
-40 to  
+85  
°C  
Sensitivity  
Untrimmed  
340  
-521  
±1  
LSB/ºC  
LSB  
Temperature Offset  
Linearity  
35oC  
Best fit straight line (-40°C to +85°C)  
°C  
VDD POWER SUPPLY  
Operating Voltages  
Power Supply Ramp Rate  
OPERATING CURRENT  
2.375  
3.465  
100  
V
Monotonic ramp. Ramp rate is 10% to 90% of the final value  
ms  
Normal Operating Current  
Gyro + Accel  
(Magnetometer and DMP disabled)  
Gyro at all rates  
3.9  
mA  
µA  
Accel + Magnetometer  
(Gyro and DMP disabled)  
Accel at 1kHz  
sample rate  
900  
Magnetometer at  
8Hz repetition rate  
Magnetometer only  
(DMP, Gyro, and Accel disabled)  
350  
µA  
Accelerometer Low Power  
Mode Current  
1.25 Hz update rate  
5 Hz update rate  
20 Hz update rate  
40 Hz update rate  
10  
20  
70  
µA  
µA  
µA  
µA  
140  
100% Duty Cycle  
Magnetometer Full Power  
Mode Current  
6
6
mA  
µA  
Full-Chip Idle Mode Supply  
Current  
VLOGIC REFERENCE  
VOLTAGE  
Voltage Range  
1.71  
-40  
VDD  
3
V
VLOGIC must be VDD at all times  
Power Supply Ramp Rate  
Monotonic ramp. Ramp rate is 10% to 90% of the final value  
ms  
Normal Operating Current  
100  
µA  
TEMPERATURE RANGE  
Specified Temperature  
Range  
Performance parameters are not applicable beyond Specified  
Temperature Range  
+85  
°C  
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6.5  
Electrical Specifications, Continued  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
PARAMETER  
CONDITIONS  
MIN  
TYP  
MAX  
Units  
Notes  
SERIAL INTERFACE  
I2C Operating Frequency  
All registers, Fast-mode  
400  
100  
kHz  
kHz  
All registers, Standard-mode  
I2C ADDRESS  
AD0 = 0  
AD0 = 1  
1101000  
1101001  
DIGITAL INPUTS (SDA, AD0,  
SCL, FSYNC, CLKIN)  
VIH, High Level Input Voltage  
VIL, Low Level Input Voltage  
0.7*VLOGIC  
0.9*VLOGIC  
V
V
0.3*VLOGIC  
CI, Input Capacitance  
< 5  
pF  
DIGITAL OUTPUT (INT)  
VOH, High Level Output Voltage  
RLOAD=1MΩ  
RLOAD=1MΩ  
V
V
V
VOL1, LOW-Level Output Voltage  
0.1*VLOGIC  
0.1  
VOL.INT1, INT Low-Level Output  
Voltage  
OPEN=1, 0.3mA sink  
Current  
Output Leakage Current  
tINT, INT Pulse Width  
OPEN=1  
100  
50  
nA  
µs  
LATCH_INT_EN=0  
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6.6  
Electrical Specifications, Continued  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
Parameters  
Conditions  
Typical  
Units  
Notes  
Primary I2C I/O (SCL, SDA)  
VIL, LOW Level Input Voltage  
VIH, HIGH-Level Input Voltage  
Vhys, Hysteresis  
-0.5V to 0.3*VLOGIC  
V
V
0.7*VLOGIC to VLOGIC + 0.5V  
0.1*VLOGIC  
V
VOL1, LOW-Level Output Voltage  
IOL, LOW-Level Output Current  
3mA sink current  
VOL = 0.4V  
0 to 0.4  
V
3
mA  
mA  
nA  
ns  
pF  
VOL = 0.6V  
5
100  
Output Leakage Current  
tof, Output Fall Time from VIHmax to VILmax  
CI, Capacitance for Each I/O pin  
Auxiliary I2C I/O (ES_CL, ES_DA)  
VIL, LOW-Level Input Voltage  
VIH, HIGH-Level Input Voltage  
Vhys, Hysteresis  
Cb bus capacitance in pF  
20+0.1Cb to 250  
< 10  
-0.5 to 0.3*VDD  
0.7*VDD to VDD+0.5V  
0.1*VDD  
V
V
V
V
VOL1, LOW-Level Output Voltage  
IOL, LOW-Level Output Current  
1mA sink current  
0 to 0.4  
VOL = 0.4V  
VOL = 0.6V  
1
1
mA  
mA  
Output Leakage Current  
100  
20+0.1Cb to 250  
< 10  
nA  
ns  
pF  
tof, Output Fall Time from VIHmax to VILmax  
CI, Capacitance for Each I/O pin  
Cb bus cap. in pF  
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6.7  
Electrical Specifications, Continued  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
Parameters  
Conditions  
Min  
Typical  
Max  
Units Notes  
INTERNAL CLOCK SOURCE  
CLK_SEL=0,1,2,3  
Gyroscope Sample Rate, Fast  
DLPFCFG=0  
SAMPLERATEDIV = 0  
8
1
1
kHz  
kHz  
kHz  
Gyroscope Sample Rate, Slow  
Accelerometer Sample Rate  
Clock Frequency Initial Tolerance  
Frequency Variation over Temperature  
PLL Settling Time  
DLPFCFG=1,2,3,4,5, or 6  
SAMPLERATEDIV = 0  
CLK_SEL=0, 25°C  
CLK_SEL=1,2,3; 25°C  
CLK_SEL=0  
-5  
-1  
+5  
+1  
%
%
-15 to +10  
%
CLK_SEL=1,2,3  
CLK_SEL=1,2,3  
±1  
1
%
ms  
EXTERNAL 32.768kHz CLOCK  
External Clock Frequency  
CLK_SEL=4  
32.768  
1 to 2  
8.192  
kHz  
µs  
External Clock Allowable Jitter  
Gyroscope Sample Rate, Fast  
Cycle-to-cycle rms  
DLPFCFG=0  
kHz  
SAMPLERATEDIV = 0  
Gyroscope Sample Rate, Slow  
Accelerometer Sample Rate  
PLL Settling Time  
DLPFCFG=1,2,3,4,5, or 6  
SAMPLERATEDIV = 0  
1.024  
1.024  
1
kHz  
kHz  
ms  
EXTERNAL 19.2MHz CLOCK  
External Clock Frequency  
CLK_SEL=5  
19.2  
MHz  
Hz  
Gyroscope Sample Rate  
Full programmable range  
3.9  
8000  
Gyroscope Sample Rate, Fast Mode  
DLPFCFG=0  
SAMPLERATEDIV = 0  
8
1
1
1
kHz  
Gyroscope Sample Rate, Slow Mode  
Accelerometer Sample Rate  
PLL Settling Time  
DLPFCFG=1,2,3,4,5, or 6  
SAMPLERATEDIV = 0  
kHz  
kHz  
ms  
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6.8  
Typical Operating Circuit of Section 7.2, VDD = 2.375V-3.465V, VLOGIC= 1.8V±5% or VDD, TA = 25°C  
I2C Timing Characterization  
Parameters  
I2C TIMING  
Conditions  
I2C FAST-MODE  
Min  
Typical  
Max  
Units  
Notes  
fSCL, SCL Clock Frequency  
400  
kHz  
µs  
tHD.STA, (Repeated) START Condition Hold  
Time  
0.6  
tLOW, SCL Low Period  
tHIGH, SCL High Period  
1.3  
0.6  
0.6  
µs  
µs  
µs  
tSU.STA, Repeated START Condition Setup  
Time  
tHD.DAT, SDA Data Hold Time  
tSU.DAT, SDA Data Setup Time  
tr, SDA and SCL Rise Time  
tf, SDA and SCL Fall Time  
0
µs  
ns  
ns  
ns  
µs  
100  
Cb bus cap. from 10 to 400pF  
Cb bus cap. from 10 to 400pF  
20+0.1Cb  
20+0.1Cb  
0.6  
300  
300  
tSU.STO, STOP Condition Setup Time  
tBUF, Bus Free Time Between STOP and  
START Condition  
1.3  
µs  
Cb, Capacitive Load for each Bus Line  
tVD.DAT, Data Valid Time  
< 400  
pF  
µs  
µs  
0.9  
0.9  
tVD.ACK, Data Valid Acknowledge Time  
I2C Bus Timing Diagram  
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6.9  
Absolute Maximum Ratings  
Stress above those listed as “Absolute Maximum Ratings” may cause permanent damage to the device.  
These are stress ratings only and functional operation of the device at these conditions is not implied.  
Exposure to the absolute maximum ratings conditions for extended periods may affect device reliability.  
Parameter  
Rating  
Supply Voltage, VDD  
VLOGIC Input Voltage Level  
REGOUT  
-0.5V to +6V  
-0.5V to VDD + 0.5V  
-0.5V to 2V  
Input Voltage Level (CLKIN, AUX_DA, AD0, FSYNC,  
INT, SCL, SDA)  
-0.5V to VDD + 0.5V  
CPOUT (2.5V VDD 3.6V )  
-0.5V to 30V  
10,000g for 0.2ms  
-40°C to +85°C  
-40°C to +125°C  
Acceleration (Any Axis, unpowered)  
Operating Temperature Range  
Storage Temperature Range  
Electrostatic Discharge (ESD) Protection  
2kV (HBM);  
250V (MM)  
Latch-up  
JEDEC Class II (2),125°C  
±100mA  
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7
Applications Information  
7.1  
Pin Out and Signal Description  
Pin Number  
Pin Name  
CLKIN  
ES_DA  
ES_CL  
VLOGIC  
AD0  
Pin Description  
1
Optional external reference clock input. Connect to GND if unused.  
Auxiliary I2C master serial data  
Auxiliary I2C Master serial clock  
6
7
8
9
Digital I/O supply voltage  
I2C Slave Address LSB (AD0)  
10  
REGOUT  
FSYNC  
INT  
Regulator filter capacitor connection  
Frame synchronization digital input. Connect to GND if unused.  
Interrupt digital output (totem pole or open-drain)  
Power supply voltage and Digital I/O supply voltage  
Power supply ground  
11  
12  
3, 13  
15, 17,18  
20  
VDD  
GND  
CPOUT  
RESV  
SCL  
Charge pump capacitor connection  
Reserved. Do not connect  
I2C serial clock (SCL)  
I2C serial data (SDA)  
22  
23  
24  
SDA  
2, 4, 5, 14,  
16, 19, 21  
RESV  
Reserved. Do not connect.  
Top View  
24 23 22 21 20 19  
+Z  
CLKIN  
RESV  
VDD  
1
2
3
4
5
6
18 GND  
17 GND  
16 RESV  
15 GND  
14 RESV  
13 VDD  
+X  
+Y  
+Z  
M
P
M
+Y  
U
P
-
9
U
1
MPU-9150  
-
9
5
0
1
5
0
RESV  
RESV  
ES_DA  
+Y  
+X  
+X  
+Z  
7
8
9
10 11 12  
Orientation of Axes of Sensitivity and  
Polarity of Rotation for Accel & Gyro  
Orientation of Axes of Sensitivity for  
Magnetometer  
LGA Package  
24-pin, 4mm x 4mm x 1mm  
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7.2  
Typical Operating Circuit  
GND  
C3  
2.2nF  
24 23 22 21 20 19  
1
2
3
4
5
6
18  
17  
16  
15  
14  
13  
CLKIN  
GND  
VDD  
MPU-9150  
VDD  
ES_DA  
ES_CL  
7
8
9
10 11 12  
C2  
0.1µF  
GND  
C1  
VLOGIC  
0.1µF  
C4  
10nF  
GND  
GND  
Typical Operating Circuit  
7.3  
Bill of Materials for External Components  
Component  
Label  
C1  
Specification  
Quantity  
Regulator Filter Capacitor (Pin 10)  
VDD Bypass Capacitor (Pin 13)  
Charge Pump Capacitor (Pin 20)  
VLOGIC Bypass Capacitor (Pin 8)  
Ceramic, X7R, 0.1µF ±10%, 2V  
Ceramic, X7R, 0.1µF ±10%, 4V  
Ceramic, X7R, 2.2nF ±10%, 50V  
Ceramic, X7R, 10nF ±10%, 4V  
1
1
1
1
C2  
C3  
C4*  
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7.4  
Recommended Power-on Procedure  
Power-Up Sequencing  
1. VLOGIC amplitude must always be ≤VDD  
amplitude  
TVDDR  
2. TVDDR is VDD rise time: Time for VDD to rise  
from 10% to 90% of its final value  
90%  
3. TVDDR is ≤100msec  
10%  
VDD  
4. TVLGR is VLOGIC rise time: Time for  
VLOGIC to rise from 10% to 90% of its final  
value  
TVLGR  
90%  
5. TVLGR is ≤3msec  
10%  
6. TVLG-VDD is the delay from the start of VDD  
ramp to the start of VLOGIC rise  
VLOGIC  
7. TVLG-VDD is 0ms;  
TVLG - VDD  
8. VDD and VLOGIC must be monotonic  
ramps  
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7.5  
Block Diagram  
1
CLKIN  
CLKOUT  
CLOCK  
Clock  
MPU-9150  
22  
Self  
test  
12  
X Accel  
Y Accel  
Z Accel  
ADC  
INT  
Interrupt  
Status  
Register  
Self  
test  
ADC  
9
AD0  
Slave I2C  
23  
24  
FIFO  
SCL  
SDA  
Self  
test  
ADC  
Config  
Registers  
7
6
Serial  
Interface  
Bypass  
Mux  
Master I2C  
Serial  
Interface  
ES_CL  
ES_DA  
Self  
test  
X Gyro  
Y Gyro  
Z Gyro  
ADC  
Sensor  
Registers  
11  
Self  
test  
FSYNC  
ADC  
Factory  
Calibration  
Digital Motion  
Processor  
(DMP)  
Self  
test  
ADC  
ADC  
Temp Sensor  
Signal Conditioning  
Charge  
Pump  
20  
CPOUT  
ADC  
ADC  
ADC  
X
Y
Z
Bias & LDO  
18  
GND  
Compass  
Compass  
Compass  
13  
VDD  
10  
REGOUT VLOGIC  
8
7.6  
Overview  
The MPU-9150 is comprised of the following key blocks and functions:  
Three-axis MEMS rate gyroscope sensor with 16-bit ADCs and signal conditioning  
Three-axis MEMS accelerometer sensor with 16-bit ADCs and signal conditioning  
Three-axis MEMS magnetometer sensor with 13-bit ADCs and signal conditioning  
Digital Motion Processor (DMP) engine  
Primary I2C serial communications interface  
Auxiliary I2C serial interface for 3rd party sensors  
Clocking  
Sensor Data Registers  
FIFO  
Interrupts  
Digital-Output Temperature Sensor  
Gyroscope, Accelerometer and Magnetometer Self-test  
Bias and LDO  
Charge Pump  
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7.7  
Three-Axis MEMS Gyroscope with 16-bit ADCs and Signal Conditioning  
The MPU-9150 includes a 3-Axis vibratory MEMS rate gyroscope, which detect rotations about the X-, Y-,  
and Z- Axes. When the gyro is are rotated about any of the sense axes, the Coriolis Effect causes a  
vibration that is detected by a capacitive pickoff. The resulting signal is amplified, demodulated, and filtered  
to produce a voltage that is proportional to the angular rate. This voltage is digitized using individual on-chip  
16-bit Analog-to-Digital Converters (ADCs) to sample each axis. The full-scale range of the gyro sensor may  
be digitally programmed to ±250, ±500, ±1000, or ±2000 degrees per second (dps). The ADC sample rate is  
programmable from 8,000 samples per second, down to 3.9 samples per second, and user-selectable low-  
pass filters enable a wide range of cut-off frequencies.  
7.8  
Three-Axis MEMS Accelerometer with 16-bit ADCs and Signal Conditioning  
The MPU-9150’s 3-axis accelerometer uses separate proof masses for each axis. Acceleration along a  
particular axis induces displacement on the corresponding proof mass, and capacitive sensors detect the  
displacement differentially. The MPU-9150’s architecture reduces the accelerometers susceptibility to  
fabrication variations as well as to thermal drift. When the device is placed on a flat surface, it will measure  
0g on the X- and Y-axes and +1g on the Z-axis. The accelerometers scale factor is calibrated at the factory  
and is nominally independent of supply voltage. Each sensor has a dedicated sigma-delta ADC for providing  
digital outputs. The full scale range of the digital output can be adjusted to ±2g, ±4g, ±8g, or ±16g.  
7.9  
Three-Axis MEMS Magnetometer with 13-bit ADCs and Signal Conditioning  
The 3-axis magnetometer uses highly sensitive Hall sensor technology. The compass portion of the IC  
incorporates magnetic sensors for detecting terrestrial magnetism in the X-, Y-, and Z- Axes, a sensor driving  
circuit, a signal amplifier chain, and an arithmetic circuit for processing the signal from each sensor. Each  
ADC has a 13-bit resolution and a full scale range of ±1200 µT.  
7.10 Digital Motion Processor  
The embedded Digital Motion Processor (DMP) is located within the MPU-9150 and offloads computation of  
motion processing algorithms from the host processor. The DMP acquires data from accelerometers,  
gyroscopes, magnetometers and additional 3rd party sensors such as pressure sensors, and processes the  
data. The resulting data can be read from the DMP’s registers, or can be buffered in a FIFO. The DMP has  
access to one of the MPU’s external pins, which can be used for generating interrupts.  
The purpose of the DMP is to offload both timing requirements and processing power from the host  
processor. Typically, motion processing algorithms should be run at a high rate, often around 200Hz, in order  
to provide accurate results with low latency. This is required even if the application updates at a much lower  
rate; for example, a low power user interface may update as slowly as 5Hz, but the motion processing should  
still run at 200Hz. The DMP can be used as a tool in order to minimize power, simplify timing, simplify the  
software architecture, and save valuable MIPS on the host processor for use in the application.  
7.11 Primary I2C  
The MPU-9150 communicates to a system processor using an I2C serial interface. The MPU-9150 always  
acts as a slave when communicating to the system processor. The logic level for communications to the  
master is set by the voltage on the VLOGIC pin. The LSB of the of the I2C slave address is set by pin 9  
(AD0).  
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7.12 Auxiliary I2C Serial Interface  
The MPU-9150 has an auxiliary I2C bus for communicating to off-chip sensors. This bus has two operating  
modes:  
I2C Master Mode: The MPU-9150 acts as a master to any external sensors connected to the  
auxiliary I2C bus  
Pass-Through Mode: The MPU-9150 directly connects the primary and auxiliary I2C buses together,  
allowing the system processor to directly communicate with any external sensors.  
Auxiliary I2C Bus Modes of Operation:  
I2C Master Mode: Allows the MPU-9150 to directly access the data registers of external digital  
sensors, such as a pressure sensor. In this mode, the MPU-9150 directly obtains data from auxiliary  
sensors, allowing the on-chip DMP to generate sensor fusion data without intervention from the  
system applications processor.  
For example, In I2C Master mode, the MPU-9150 can be configured to perform burst reads, returning  
the following data from a triple-Axis external sensor:  
.
.
.
X-Axis data (2 bytes)  
Y-Axis data (2 bytes)  
Z-Axis data (2 bytes)  
The I2C Master can be configured to read up to 24 bytes from up to 3 auxiliary sensors. A fourth  
sensor can be configured to work single byte read/write mode.  
Pass-Through Mode: Allows an external system processor to act as master and directly  
communicate to the external sensors connected to the auxiliary I2C bus pins (ES_DA and ESCL). In  
this mode, the auxiliary I2C bus control logic (3rd-party sensor interface block) of the MPU-9150 is  
disabled, and the auxiliary I2C pins ES_DA and ES_CL (Pins 6 and 7) are connected to the main I2C  
bus (Pins 23 and 24) through analog switches.  
Pass-Through Mode is useful for configuring the external sensor, or for keeping the MPU-9150 in a  
low-power mode when only the external sensors are used. In Pass-Through Mode the system  
processor can still access MPU-9150 data through the I2C interface.  
Auxiliary I2C Bus IO Logic Level  
The logic level of the auxiliary I2C bus is VDD.  
For further information regarding the MPU-9150’s logic level, please refer to Section 10.2.  
7.13 Self-Test  
Please refer to the MPU-9150 self-test applications note and MPU-9150 register map for more details on  
self-test.  
Self-test allows for the testing of the mechanical and electrical portions of the sensors. The self-test for each  
measurement axis can be activated by controlling the bits of the Gyro and Accel control registers.  
When self-test is activated, the electronics cause the sensors to be actuated and produce an output signal.  
The output signal is used to observe the self-test response.  
The self-test response is defined as follows:  
Self-test response = Sensor output with self-test enabled Sensor output without self-test enabled  
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The self-test response for each accelerometer axis is defined in the accelerometer specification table  
(Section 6.2), while that for each gyroscope axis is defined in the gyroscope specification table (Section 6.1).  
When the value of the self-test response is within the min/max limits of the product specification, the part has  
passed self-test. When the self-test response exceeds the min/max values, the part is deemed to have  
failed self-test. Code for operating self-test code is included within the MotionApps software provided by  
InvenSense.  
7.14 MPU-9150 Solution for 10-Axis Sensor Fusion Using I2C Interface  
In the figure below, the system processor is an I2C master to the MPU-9150. In addition, the MPU-9150 is an  
I2C master to the optional external pressure sensor. The MPU-9150 has limited capabilities as an I2C Master,  
and depends on the system processor to manage the initial configuration of any auxiliary sensors. The MPU-  
9150 has an interface bypass multiplexer, which connects the system processor I2C bus pins 23 and 24  
(SDA and SCL) directly to the auxiliary sensor I2C bus pins 6 and 7 (ES_DA and ES_CL).  
Once the auxiliary sensors have been configured by the system processor, the interface bypass multiplexer  
should be disabled so that the MPU-9150 auxiliary I2C master can take control of the sensor I2C bus and  
gather data from the auxiliary sensors.  
For further information regarding I2C master control, please refer to Section 10.  
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I2C Processor Bus: for reading all  
sensor data from MPU and for  
configuring external sensors (i.e.  
compass in this example)  
Interrupt  
12  
INT  
Status  
Register  
8
9
/CS  
VDD  
VDD or GND  
MPU-9150  
AD0/SDO  
Slave I2C  
or SPI  
Serial  
Interface  
23  
SCL/SCLK  
SDA/SDI  
SCL  
SDA  
System  
Processor  
24  
FIFO  
Sensor I2C Bus: for  
configuring and reading  
from external sensors  
Config  
Register  
Optional  
Sensor  
Master I2C  
Serial  
7
6
ES_CL  
ES_DA  
SCL  
SDA  
Sensor  
Register  
Interface  
Bypass  
Mux  
Pressure  
Sensor  
Interface  
Factory  
Calibration  
Digital  
Motion  
Processor  
(DMP)  
Interface bypass mux allows  
direct configuration of  
compass by system processor  
Bias & LDO  
18  
13  
VDD  
10  
REGOUT  
GND  
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7.15 Procedure for Directly Accessing the AK8975 3-Axis Compass  
The AK8975 3-Axis Compass is connected to the MPU-9150 through the MPU’s Auxiliary I2C Bus. In order to  
access this compass directly, the MPU-9150 should be put into Pass-Through Mode.  
For further information regarding MPU-9150 Pass-Through Mode, please refer to Section 7.12.  
The slave address for AK8975 is 0x0C or 12 decimal.  
The MPU-9150 pin configuration for Direct Access to the AK8975 is described in the table below.  
Pin Configuration for Direct Access to AK8975 3-Axis Compass  
Pin Number  
Pin Name  
CLKIN  
Pin Description  
1
6
Inactive. Connect to GND.  
Active. Leave as NC.  
ES_DA  
(provision for option external pull-up resistor to VDD)  
7
ES_CL  
Active. Leave as NC.  
(provision for option external pull-up resistor to VDD)  
8
9
VLOGIC  
AD0  
Active. Digital I/O supply voltage.  
Active. Connect to GND.  
10  
REGOUT  
FSYNC  
INT  
Active. Connect a 100nF bypass capacitor on the board.  
Inactive. Connect to GND.  
11  
12  
Inactive. Leave as NC.  
3, 13  
15, 17,18  
20  
VDD  
Power supply voltage and Digital I/O supply voltage  
Power supply ground.  
GND  
CPOUT  
RESV  
SCL  
Active. Connect a 10nF bypass capacitor on the board.  
Reserved. Do not connect.  
Active. I2C serial clock (SCL)  
Active. I2C serial data (SDA)  
22  
23  
24  
SDA  
2, 4, 5, 14,  
16, 19, 21  
RESV  
Reserved. Do not connect.  
For detailed information regarding the Register Map of the AK8975, please refer to the MPU-9150 Register  
Map and Register Descriptions document.  
7.16 Internal Clock Generation  
The MPU-9150 has a flexible clocking scheme, allowing a variety of internal or external clock sources to be  
used for the internal synchronous circuitry. This synchronous circuitry includes the signal conditioning and  
ADCs, the DMP, and various control circuits and registers. An on-chip PLL provides flexibility in the  
allowable inputs for generating this clock.  
Allowable internal sources for generating the internal clock are:  
An internal relaxation oscillator  
Any of the X, Y, or Z gyros (MEMS oscillators with a variation of ±1% over temperature)  
Allowable external clocking sources are:  
32.768kHz square wave  
19.2MHz square wave  
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Selection of the source for generating the internal synchronous clock depends on the availability of external  
sources and the requirements for power consumption and clock accuracy. These requirements will most  
likely vary by mode of operation. For example, in one mode, where the biggest concern is power  
consumption, the user may wish to operate the Digital Motion Processor of the MPU-9150 to process  
accelerometer data, while keeping the gyros and magnetometer off. In this case, the internal relaxation  
oscillator is a good clock choice. However, in another mode, where the gyros are active, selecting the gyros  
as the clock source provides for a more accurate clock source.  
Clock accuracy is important, since timing errors directly affect the distance and angle calculations performed  
by the Digital Motion Processor (and by extension, by any processor).  
There are also start-up conditions to consider. When the MPU-9150 first starts up, the device uses its  
internal clock until programmed to operate from another source. This allows the user, for example, to wait  
for the MEMS oscillators to stabilize before they are selected as the clock source.  
7.17 Sensor Data Registers  
The sensor data registers contain the latest gyro, accelerometer, magnetometer, and temperature  
measurement data. They are read-only registers, and are accessed via the serial interface. Data from these  
registers may be read anytime. However, the interrupt function may be used to determine when new data is  
available.  
For a table of interrupt sources please refer to Section 8.  
7.18 FIFO  
The MPU-9150 contains a 1024-byte FIFO register that is accessible via the Serial Interface. The FIFO  
configuration register determines which data is written into the FIFO. Possible choices include gyro data,  
accelerometer data, temperature readings, auxiliary sensor readings, and FSYNC input. A FIFO counter  
keeps track of how many bytes of valid data are contained in the FIFO. The FIFO register supports burst  
reads. The interrupt function may be used to determine when new data is available.  
For further information regarding the FIFO, please refer to the MPU-9150 Register Map and Register  
Descriptions document.  
7.19 Interrupts  
Interrupt functionality is configured via the Interrupt Configuration register. Items that are configurable include  
the INT pin configuration, the interrupt latching and clearing method, and triggers for the interrupt. Items that  
can trigger an interrupt are (1) new data is available to be read (from the FIFO and Data registers); (2)  
accelerometer event interrupts; and (3) the MPU-9150 did not receive an acknowledge from an auxiliary  
sensor on the secondary I2C bus. The interrupt status can be read from the Interrupt Status register.  
For further information regarding interrupts, please refer to the MPU-9150 Register Map and Register  
Descriptions document.  
For information regarding the MPU-9150’s accelerometer event interrupts, please refer to Section 8.  
7.20 Digital-Output Temperature Sensor  
An on-chip temperature sensor and ADC are used to measure the MPU-9150 die temperature. The readings  
from the ADC can be read from the FIFO or the Sensor Data registers.  
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7.21 Bias and LDO  
The bias and LDO section generates the internal supply and the reference voltages and currents required by  
the MPU-9150. Its two inputs are an unregulated VDD and a VLOGIC logic reference supply voltage. The  
LDO output is bypassed by a capacitor at REGOUT. For further details on the capacitor, please refer to the  
Bill of Materials for External Components (Section 7.3).  
7.22 Charge Pump  
An on-board charge pump generates the high voltage required for the MEMS oscillators. Its output is  
bypassed by a capacitor at CPOUT. For further details on the capacitor, please refer to the Bill of Materials  
for External Components (Section 7.3).  
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8
Programmable Interrupts  
The MPU-9150 has a programmable interrupt system which can generate an interrupt signal on the INT pin.  
Status flags indicate the source of an interrupt. Interrupt sources may be enabled and disabled individually.  
Table of Interrupt Sources  
Interrupt Name  
Module  
FIFO Overflow  
FIFO  
Data Ready  
Sensor Registers  
I2C Master  
I2C Master  
I2C Master errors: Lost Arbitration, NACKs  
I2C Slave 4  
For information regarding the interrupt enable/disable registers and flag registers, please refer to the MPU-  
9150 Register Map and Register Descriptions document.  
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9
Digital Interface  
I2C Serial Interface  
9.1  
The internal registers and memory of the MPU-9150 can be accessed using either I2C at 400 kHz.  
Serial Interface  
Pin Number  
Pin Name  
VLOGIC  
AD0  
Pin Description  
8
9
Digital I/O supply voltage. VLOGIC must be VDD at all times.  
I2C Slave Address LSB  
I2C serial clock  
I2C serial data  
23  
24  
SCL  
SDA  
9.2  
I2C Interface  
I2C is a two-wire interface comprised of the signals serial data (SDA) and serial clock (SCL). In general, the  
lines are open-drain and bi-directional. In a generalized I2C interface implementation, attached devices can  
be a master or a slave. The master device puts the slave address on the bus, and the slave device with the  
matching address acknowledges the master.  
The MPU-9150 always operates as a slave device when communicating to the system processor, which thus  
acts as the master. SDA and SCL lines typically need pull-up resistors to VDD. The maximum bus speed is  
400 kHz.  
The slave address of the MPU-9150 is b110100X which is 7 bits long. The LSB bit of the 7 bit address is  
determined by the logic level on pin AD0. This allows two MPU-9150s to be connected to the same I2C bus.  
When used in this configuration, the address of the one of the devices should be b1101000 (pin AD0 is logic  
low) and the address of the other should be b1101001 (pin AD0 is logic high).  
9.3  
I2C Communications Protocol  
START (S) and STOP (P) Conditions  
Communication on the I2C bus starts when the master puts the START condition (S) on the bus, which is  
defined as a HIGH-to-LOW transition of the SDA line while SCL line is HIGH (see figure below). The bus is  
considered to be busy until the master puts a STOP condition (P) on the bus, which is defined as a LOW to  
HIGH transition on the SDA line while SCL is HIGH (see figure below).  
Additionally, the bus remains busy if a repeated START (Sr) is generated instead of a STOP condition.  
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SDA  
SCL  
S
P
START condition  
STOP condition  
START and STOP Conditions  
Data Format / Acknowledge  
I2C data bytes are defined to be 8-bits long. There is no restriction to the number of bytes transmitted per  
data transfer. Each byte transferred must be followed by an acknowledge (ACK) signal. The clock for the  
acknowledge signal is generated by the master, while the receiver generates the actual acknowledge signal  
by pulling down SDA and holding it low during the HIGH portion of the acknowledge clock pulse.  
If a slave is busy and cannot transmit or receive another byte of data until some other task has been  
performed, it can hold SCL LOW, thus forcing the master into a wait state. Normal data transfer resumes  
when the slave is ready, and releases the clock line (refer to the following figure).  
DATA OUTPUT BY  
TRANSMITTER (SDA)  
not acknowledge  
DATA OUTPUT BY  
RECEIVER (SDA)  
acknowledge  
SCL FROM  
MASTER  
1
2
8
9
clock pulse for  
acknowledgement  
START  
condition  
Acknowledge on the I2C Bus  
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Communications  
After beginning communications with the START condition (S), the master sends a 7-bit slave address  
followed by an 8th bit, the read/write bit. The read/write bit indicates whether the master is receiving data from  
or is writing to the slave device. Then, the master releases the SDA line and waits for the acknowledge  
signal (ACK) from the slave device. Each byte transferred must be followed by an acknowledge bit. To  
acknowledge, the slave device pulls the SDA line LOW and keeps it LOW for the high period of the SCL line.  
Data transmission is always terminated by the master with a STOP condition (P), thus freeing the  
communications line. However, the master can generate a repeated START condition (Sr), and address  
another slave without first generating a STOP condition (P). A LOW to HIGH transition on the SDA line while  
SCL is HIGH defines the stop condition. All SDA changes should take place when SCL is low, with the  
exception of start and stop conditions.  
SDA  
SCL  
1 7  
8
9
1 7  
8
9
1 7  
8
9
S
P
START  
STOP  
ADDRESS  
R/W  
ACK  
DATA  
ACK  
DATA  
ACK  
condition  
condition  
Complete I2C Data Transfer  
To write the internal MPU-9150 registers, the master transmits the start condition (S), followed by the I2C  
address and the write bit (0). At the 9th clock cycle (when the clock is high), the MPU-9150 acknowledges the  
transfer. Then the master puts the register address (RA) on the bus. After the MPU-9150 acknowledges the  
reception of the register address, the master puts the register data onto the bus. This is followed by the ACK  
signal, and data transfer may be concluded by the stop condition (P). To write multiple bytes after the last  
ACK signal, the master can continue outputting data rather than transmitting a stop signal. In this case, the  
MPU-9150 automatically increments the register address and loads the data to the appropriate register. The  
following figures show single and two-byte write sequences.  
Single-Byte Write Sequence  
Master  
Slave  
S
AD+W  
RA  
RA  
DATA  
DATA  
P
ACK  
ACK  
ACK  
ACK  
ACK  
ACK  
Burst Write Sequence  
Master  
Slave  
S
AD+W  
DATA  
P
ACK  
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To read the internal MPU-9150 registers, the master sends a start condition, followed by the I2C address and  
a write bit, and then the register address that is going to be read. Upon receiving the ACK signal from the  
MPU-9150, the master transmits a start signal followed by the slave address and read bit. As a result, the  
MPU-9150 sends an ACK signal and the data. The communication ends with a not acknowledge (NACK)  
signal and a stop bit from master. The NACK condition is defined such that the SDA line remains high at the  
9th clock cycle. The following figures show single and two-byte read sequences.  
Single-Byte Read Sequence  
Master  
Slave  
S
AD+W  
RA  
RA  
S
S
AD+R  
AD+R  
NACK  
ACK  
P
ACK  
ACK  
ACK  
ACK  
ACK DATA  
ACK DATA  
Burst Read Sequence  
Master  
Slave  
S
AD+W  
NACK  
P
DATA  
9.4  
I2C Terms  
Signal Description  
S
AD  
W
Start Condition: SDA goes from high to low while SCL is high  
Slave I2C address  
Write bit (0)  
R
Read bit (1)  
ACK  
Acknowledge: SDA line is low while the SCL line is high at the  
9th clock cycle  
NACK Not-Acknowledge: SDA line stays high at the 9th clock cycle  
RA  
DATA  
P
MPU-9150 internal register address  
Transmit or received data  
Stop condition: SDA going from low to high while SCL is high  
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10 Serial Interface Considerations  
10.1 MPU-9150 Supported Interfaces  
The MPU-9150 supports I2C communications.  
10.2 Logic Levels  
The MPU-9150’s I/O logic levels are set to be either VDD or VLOGIC, as shown in the table below.  
I/O Logic Levels  
MICROPROCESSOR LOGIC LEVELS  
AUXILIARY LOGIC LEVELS  
(Pins: SDA, SCL, AD0, CLKIN, INT)  
(Pins: ES_DA, ES_CL)  
VLOGIC  
VDD  
VLOGIC may be set to be equal to VDD or to another voltage. However, VLOGIC must be ≤ VDD at all  
times. VLOGIC is the power supply voltage for the microprocessor system bus and VDD is the supply for the  
auxiliary I2C bus, as shown in the figure of Section 10.3.  
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10.3 Logic Levels Diagram  
The figure below depicts a sample circuit with a third party pressure sensor attached to the auxiliary I2C bus.  
It shows logic levels and voltage connections. Note: Actual configuration will depend on the auxiliary sensors  
used.  
VLOGIC  
VDD_IO  
(0V - VLOGIC)  
SYSTEM BUS  
System  
Processor  
IO  
VDD  
VLOGIC  
(0V - VLOGIC)  
VDD  
INT  
(0V - VLOGIC)  
(0V - VLOGIC)  
VLOGIC  
SDA  
SCL  
(0V - VLOGIC)  
(0V - VLOGIC)  
CLKIN  
VDD  
FSYNC  
VLOGIC  
MPU-9150  
VDD  
VLOGIC  
AD0  
INT 1  
(0V - VLOGIC)  
(0V - VLOGIC)  
INT 2  
0V - VDD  
0V - VDD  
ES_DA  
ES_CL  
SDA  
SCL  
(0V, VLOGIC)  
0V - VDD  
ADDR  
3rd Party  
Pressure sensor  
I/O Levels and Connections  
Notes:  
1. The IO voltage levels of ES_DA and ES_CL are set relative to VDD.  
2. Third-party auxiliary device logic levels are referenced to VDD. Setting INT1 and INT2 to open drain  
configuration provides voltage compatibility when VDD ≠ VLOGIC. When VDD = VLOGIC, INT1 and  
INT2 may be set to push-pull outputs, and external pull-up resistors are not needed.  
3. All other MPU-9150 logic IO is always referenced to VLOGIC.  
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11 Assembly  
This section provides general guidelines for assembling InvenSense Micro Electro-Mechanical Systems  
(MEMS) gyros packaged in Lead Grid Array package (LGA) surface mount integrated circuits.  
11.1 Orientation of Axes  
The diagram below shows the orientation of the axes of sensitivity and the polarity of rotation. Note the pin 1  
identifier () in the figure.  
+Z  
+Y  
M
P
U
-
9
1
5
0
+X  
Orientation of Axes of Sensitivity  
and Polarity of Rotation for  
Gyroscopes and Accelerometers  
+X  
M
P
U
-
9
1
5
0
+Y  
+Z  
Orientation of Axes of Sensitivity  
for Compass  
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11.2 Package Dimensions  
SYMBOLS  
DIMENSIONS IN MILLIMETERS  
MIN.  
NOM.  
MAX.  
0.90  
0.106  
3.90  
3.90  
---  
---  
---  
0.22  
0.22  
0.32  
---  
1.00  
0.136  
4.00  
4.00  
2.50  
3.41  
0.50  
0.25  
0.25  
0.35  
0.12  
0.35  
1.10  
0.166  
4.10  
4.10  
---  
---  
---  
0.28  
0.28  
0.38  
---  
A
c
D
E
D1/E1  
D2/E2  
e
b
f
L
s
0.32  
0.38  
x
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11.3 PCB Design Guidelines:  
The Pad Diagram using a JEDEC type extension with solder rising on the outer edge is shown below. The  
Pad Dimensions Table shows pad sizing (mean dimensions) recommended for the MPU-9150 product.  
JEDEC type extension with solder rising on outer edge  
PCB Lay-out Diagram  
SYMBOLS  
DIMENSIONS IN MILLIMETERS  
NOM  
Nominal Package I/O Pad Dimensions  
e
b
L1  
L3  
D
Pad Pitch  
Pad Width  
Pad Length  
Pad Length  
0.50  
0.25  
0.35  
0.40  
4.00  
4.00  
Package Width  
E
Package Length  
I/O Land Design Dimensions (Guidelines )  
I/O Pad Extent Width  
I/O Pad Extent Length  
Land Width  
Outward Extension  
Inward Extension  
Land Length  
D2  
E2  
c
Tout  
Tin  
L2  
4.80  
4.80  
0.35  
0.40  
0.05  
0.80  
0.85  
L4  
Land Length  
PCB Dimensions Table (for PCB Lay-out Diagram)  
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11.4 Assembly Precautions  
11.4.1 Surface Mount Guidelines  
InvenSense MEMS motion sensors are sensitive to mechanical stress coming from the printed circuit board  
(PCB). This PCB stress can be minimized by adhering to certain design rules.  
When using MEMS components in plastic packages, PCB mounting and assembly can cause package  
stress. This package stress in turn can affect the output offset and its value over a wide range of  
temperatures. This stress is caused by the mismatch between the Coefficient of Linear Thermal Expansion  
(CTE) of the package material and the PCB. Care must be taken to avoid package stress due to mounting.  
Traces connected to pads should be as symmetric as possible. Maximizing symmetry and balance for pad  
connection will help component self alignment and will lead to better control of solder paste reduction after  
reflow.  
Any material used in the surface mount assembly process of the MEMS product should be free of restricted  
RoHS elements or compounds. Pb-free solders should be used for assembly.  
11.4.2 Exposed Die Pad Precautions  
The MPU-9150 has very low active and standby current consumption. The exposed center die pad is not  
required for heat sinking, and should not be soldered to the PCB. Under-fill should also not be used. Failure  
to adhere to this rule can induce performance changes due to package thermo-mechanical stress. There is  
no electrical connection between the pad and the CMOS.  
11.4.3 Trace Routing  
Routing traces or vias under the gyro package such that they run under the exposed die pad is prohibited.  
Routed active signals may harmonically couple with the gyro MEMS devices, compromising gyro response.  
These devices are designed with the drive frequencies as follows: X = 33±3kHz, Y = 30±3kHz, and  
Z=27±3kHz. To avoid harmonic coupling don’t route active signals in non-shielded signal planes directly  
below, or above the gyro package. Note: For best performance, design a ground plane under the e-pad to  
reduce PCB signal noise from the board on which the gyro device is mounted. If the gyro device is stacked  
under an adjacent PCB board, design a ground plane directly above the gyro device to shield active signals  
from the adjacent PCB board.  
11.4.4 Component Placement  
Do not place large insertion components such as keyboard or similar buttons, connectors, or shielding boxes  
at a distance of less than 6 mm from the MEMS gyro. Maintain generally accepted industry design practices  
for component placement near the MPU-9150 to prevent noise coupling and thermo-mechanical stress.  
11.4.5 PCB Mounting and Cross-Axis Sensitivity  
Orientation errors of the gyroscope and accelerometer mounted to the printed circuit board can cause cross-  
axis sensitivity in which one gyro or accel responds to rotation or acceleration about another axis,  
respectively. For example, the X-axis gyroscope may respond to rotation about the Y or Z axes. The  
orientation mounting errors are illustrated in the figure below.  
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Z
Φ
Y
M
P
U
-
9
1
5
0
X
Θ
Package Gyro & Accel Axes (  
) Relative to PCB Axes (  
) with Orientation Errors (Θ and Φ)  
The table below shows the cross-axis sensitivity as a percentage of the specified gyroscope or  
accelerometer’s sensitivity for a given orientation error, respectively.  
Cross-Axis Sensitivity vs. Orientation Error  
Orientation Error  
Cross-Axis Sensitivity  
(θ or Φ)  
0º  
(sinθ or sinΦ)  
0%  
0.5º  
1º  
0.87%  
1.75%  
The specifications for cross-axis sensitivity in Section 6.1 and Section 6.2 include the effect of the die  
orientation error with respect to the package.  
11.4.6 MEMS Handling Instructions  
MEMS (Micro Electro-Mechanical Systems) are a time-proven, robust technology used in hundreds of  
millions of consumer, automotive and industrial products. MEMS devices consist of microscopic moving  
mechanical structures. They differ from conventional IC products, even though they can be found in similar  
packages. Therefore, MEMS devices require different handling precautions than conventional ICs prior to  
mounting onto printed circuit boards (PCBs).  
The MPU-9150 has been qualified to a shock tolerance of 10,000g. InvenSense packages its gyroscopes as  
it deems proper for protection against normal handling and shipping. It recommends the following handling  
precautions to prevent potential damage.  
Do not drop individually packaged gyroscopes, or trays of gyroscopes onto hard surfaces. Components  
placed in trays could be subject to g-forces in excess of 10,000g if dropped.  
Printed circuit boards that incorporate mounted gyroscopes should not be separated by manually  
snapping apart. This could also create g-forces in excess of 10,000g.  
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Do not clean MEMS gyroscopes in ultrasonic baths. Ultrasonic baths can induce MEMS damage if the  
bath energy causes excessive drive motion through resonant frequency coupling.  
11.4.7 ESD Considerations  
Establish and use ESD-safe handling precautions when unpacking and handling ESD-sensitive devices.  
Store ESD sensitive devices in ESD safe containers until ready for use. The Tape-and-Reel moisture-  
sealed bag is an ESD approved barrier. The best practice is to keep the units in the original moisture  
sealed bags until ready for assembly.  
Restrict all device handling to ESD protected work areas that measure less than 200V static charge.  
Ensure that all workstations and personnel are properly grounded to prevent ESD.  
11.5 Reflow Specification  
Qualification Reflow: The MPU-9150 was qualified in accordance with IPC/JEDEC J-STD-020D.1. This  
standard classifies proper packaging, storage and handling in order to avoid subsequent thermal and  
mechanical damage during the solder reflow attachment phase of PCB assembly.  
The qualification preconditioning process specifies a sequence consisting of a bake cycle, a moisture soak  
cycle (in a temperature humidity oven), and three consecutive solder reflow cycles, followed by functional  
device testing.  
The peak solder reflow classification temperature requirement for package qualification is (260 +5/-0°C) for  
lead-free soldering of components measuring less than 1.6 mm in thickness. The qualification profile and a  
table explaining the set-points are shown below:  
SOLDER REFLOW PROFILE FOR QUALIFICATION  
LEAD-FREE IR/CONVECTION  
F
TPmax  
TPmin  
E
G
10-30sec  
H
D
TLiquidus  
Tsmax  
C
Liquidus  
60-120sec  
Tramp-up  
( < 3 C/sec)  
B
I
Tramp-down  
( < 4 C/sec)  
Tsmin  
Preheat  
60-120sec  
Troom-Pmax  
(< 480sec)  
A
Time [Seconds]  
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Temperature Set Points Corresponding to Reflow Profile Above  
CONSTRAINTS  
Step Setting  
Temp (°C)  
Time (sec)  
Max. Rate (°C/sec)  
A
B
C
D
Troom  
TSmin  
TSmax  
TLiquidus  
25  
150  
200  
217  
60 < tBC < 120  
r(TLiquidus-TPmax) < 3  
r(TLiquidus-TPmax) < 3  
r(TLiquidus-TPmax) < 3  
r(TPmax-TLiquidus) < 4  
E
TPmin  
255  
[255°C, 260°C]  
F
G
TPmax  
TPmin  
260  
255  
tAF < 480  
10< tEG < 30  
[ 260°C, 265°C]  
[255°C, 260°C]  
H
I
TLiquidus  
Troom  
217  
25  
60 < tDH < 120  
Notes: Customers must never exceed the Classification temperature (TPmax = 260°C).  
All temperatures refer to the topside of the QFN package, as measured on the package body surface.  
Production Reflow: Check the recommendations of your solder manufacturer. For optimum results, use  
lead-free solders that have lower specified temperature profiles (Tpmax ~ 235°C). Also use lower ramp-up and  
ramp-down rates than those used in the qualification profile. Never exceed the maximum conditions that we  
used for qualification, as these represent the maximum tolerable ratings for the device.  
11.6 Storage Specifications  
The storage specification of the MPU-9150 conforms to IPC/JEDEC J-STD-020D.1 Moisture Sensitivity Level  
(MSL) 3.  
Calculated shelf-life in moisture-sealed bag 12 months -- Storage conditions: <40°C and <90% RH  
After opening moisture-sealed bag  
168hours -- Storage conditions: ambient ≤30°C at 60%RH  
11.7 Package Marking Specification  
TOP VIEW  
InvenSense  
MPU9150  
Part number  
Lot traceability code  
XXXXXX-XX  
XX YYWW X  
Foundry code  
Package Vendor Code  
Rev Code  
YY = Year Code  
WW = Work Week  
Package Marking Specification  
Proprietary and Confidential  
44 of 50  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
11.8 Tape & Reel Specification  
Tape Dimensions  
Reel Outline Drawing  
Reel Dimensions and Package Size  
PACKAGE  
REEL (mm)  
SIZE  
4x4  
L
V
W
Z
330  
102  
12.8  
2.3  
Proprietary and Confidential  
45 of 50  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
Package Orientation  
User Direction  
of Feed  
Pin 1  
INVENSENSE  
INVENSENSE  
Cover Tape  
(Anti-Static)  
Carrier Tape  
(Anti-Static)  
Reel  
Terminal Tape  
Label  
Tape and Reel Specification  
Reel Specifications  
Quantity Per Reel  
Reels per Box  
5,000  
1
5
Boxes Per Carton (max)  
Pcs/Carton (max)  
25,000  
11.9 Label  
Location of Label  
Proprietary and Confidential  
46 of 50  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
11.10 Packaging  
REEL with Barcode &  
Caution labels  
Vacuum-Sealed Moisture  
Barrier Bag with ESD, MSL3,  
Caution, and Barcode Labels  
MSL3 Label  
Caution Label  
ESD Label  
Inner Bubble Wrap  
Pizza Box  
Pizza Boxes Placed in Foam-  
Lined Shipper Box  
Outer Shipper Label  
Proprietary and Confidential  
47 of 50  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
11.11 Representative Shipping Carton Label  
Proprietary and Confidential  
48 of 50  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
12 Reliability  
12.1 Qualification Test Policy  
InvenSense’s products complete a Qualification Test Plan before being released to production. The  
Qualification Test Plan for the MPU-9150 followed the JESD 47I Standards, “Stress-Test-Driven Qualification  
of Integrated Circuits,” with the individual tests described below.  
12.2 Qualification Test Plan  
Accelerated Life Tests  
TEST  
Method/Condition  
Lot  
Quantity  
Sample /  
Lot  
Acc /  
Reject  
Criteria  
(HTOL/LFR)  
High Temperature Operating Life  
JEDEC JESD22-A108D  
Dynamic, 3.63V biased, Tj>125°C  
[read-points 168, 500, 1000 hours]  
3
3
3
77  
77  
77  
(0/1)  
(0/1)  
(0/1)  
(HAST)  
JEDEC JESD22-A118A  
Condition A, 130°C, 85%RH, 33.3 psia., unbiased,  
[read-point 96 hours]  
Highly Accelerated Stress Test (1)  
(HTS)  
JEDEC JESD22-A103D  
High Temperature Storage Life  
Condition A, 125°C Non-Bias Bake  
[read-points 168, 500, 1000 hours]  
Device Component Level Tests  
Method/Condition  
TEST  
Lot  
Quantity  
Sample /  
Lot  
Acc /  
Reject  
Criteria  
(ESD-HBM)  
ESD-Human Body Model  
JEDEC JS-001-2012  
(2KV)  
1
3
(0/1)  
(ESD-MM)  
ESD-Machine Model  
JEDEC JESD22-A115C  
(250V)  
1
1
3
3
6
5
(0/1)  
(0/1)  
(0/1)  
(LU)  
Latch Up  
JEDEC JESD-78D  
Class II (2), 125°C; ±100mA  
(MS)  
Mechanical Shock  
JEDEC JESD22-B104C, Mil-Std-883  
Method 2002.5, Cond. E, 10,000g’s, 0.2ms,  
±X, Y, Z 6 directions, 5 times/direction  
(VIB)  
Vibration  
JEDEC JESD22-B103B  
Variable Frequency (random), Cond. B, 5-500Hz,  
X, Y, Z 4 times/direction  
1
3
5
(0/1)  
(0/1)  
(TC)  
JEDEC JESD22-A104D  
Condition G [-40°C to +125°C],  
Soak Mode 2 [5’],  
77  
Temperature Cycling (1)  
[Read-Points 1000 cycles]  
(1) Tests are preceded by MSL3 Preconditioning in accordance with JEDEC JESD22-A113F  
Proprietary and Confidential  
49 of 50  
Document Number: PS-MPU-9150A-00  
Revision: 4.3  
Release Date: 9/18/2013  
MPU-9150 Product Specification  
13 Environmental Compliance  
The MPU-9150 is RoHS and Green compliant.  
The MPU-9150 is in full environmental compliance as evidenced in report HS-MPU-9150, Materials  
Declaration Data Sheet.  
Environmental Declaration Disclaimer:  
InvenSense believes this environmental information to be correct but cannot guarantee accuracy or completeness. Conformity  
documents for the above component constitutes are on file. InvenSense subcontracts manufacturing and the information contained  
herein is based on data received from vendors and suppliers, which has not been validated by InvenSense.  
This information furnished by InvenSense is believed to be accurate and reliable. However, no responsibility is assumed by InvenSense  
for its use, or for any infringements of patents or other rights of third parties that may result from its use. Specifications are subject to  
change without notice. InvenSense reserves the right to make changes to this product, including its circuits and software, in order to  
improve its design and/or performance, without prior notice. InvenSense makes no warranties, neither expressed nor implied, regarding  
the information and specifications contained in this document. InvenSense assumes no responsibility for any claims or damages arising  
from information contained in this document, or from the use of products and services detailed therein. This includes, but is not limited  
to, claims or damages based on the infringement of patents, copyrights, mask work and/or other intellectual property rights.  
Certain intellectual property owned by InvenSense and described in this document is patent protected. No license is granted by  
implication or otherwise under any patent or patent rights of InvenSense. This publication supersedes and replaces all information  
previously supplied. Trademarks that are registered trademarks are the property of their respective companies. InvenSense sensors  
should not be used or sold in the development, storage, production or utilization of any conventional or mass-destructive weapons or for  
any other weapons or life threatening applications, as well as in any other life critical applications such as medical equipment,  
transportation, aerospace and nuclear instruments, undersea equipment, power plant equipment, disaster prevention and crime  
prevention equipment.  
InvenSense®, MotionCommand®, TouchAnywhere®, and AirSign® are registered trademarks of InvenSense, Inc. MPU™, MPU-  
9150™, Motion Processing Unit, MotionFusion™, MotionProcessing™, MotionApps™, Digital Motion Processor™, Digital Motion  
Processing, DMP™, BlurFree™, and InstantGesture™ are trademarks of InvenSense, Inc.  
©2013 InvenSense, Inc. All rights reserved.  
Proprietary and Confidential  
50 of 50  

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