AT7910EKB-E [ATMEL]
SpW-10X SpaceWire Router; SPW- 10X的SpaceWire路由器型号: | AT7910EKB-E |
厂家: | ATMEL |
描述: | SpW-10X SpaceWire Router |
文件: | 总19页 (文件大小:284K) |
中文: | 中文翻译 | 下载: | 下载PDF数据表文档文件 |
Features
• SpaceWire Router
– Logical to Physical addressing translation
– Priority Management
– Header Deletion Capability
• Eight Bidirectional SpaceWire links
– Full duplex communication
– Data rate from 2 up to 200 Mbit/s in each direction
• Two External Interfaces
SpW-10X
SpaceWire
Router
– Dedicated Input and Output FIFOs
– 9-bit wide Interface
• Configuration Port
– Read/Write Accesses to internal registers
– Accessible from both the spacewire links (8 channels) and the external interfaces
– Remote Memory Access Protocol (RMAP) support
• Time Code Interface
AT7910E
– Master/Slave Capability
• Error/Status Interface
• Operating range
– Voltages
• 3V to 3.6V
– Temperature
• - 55°C to +125°C
• Maximum Power consumption
– All spacewire links active at 200Mbit/s : 4W -TBC
• Radiation Performance
– Total dose tested successfully up to 300 Krad (Si)
– No single event latchup below a LET of 80 MeV/mg/cm2
• ESD better than 2000V
• Quality Grades
– QML-Q or V with SMD
• Package: 196pins MQFPF
• Mass: 12grams
7796B–AERO–08/08
1. Description
The SpW-10X SpaceWire routing switch is capable of connecting many nodes, providing a
means of routing packets between the nodes connected to it. It comprises eight SpaceWire link
interfaces and a routing matrix. The routing matrix enables packets arriving at one link interface
to be transferred to and sent out of another link interface on the routing switch.
The AT7910E was designed by Austrian Aerospace (Austria) and the University of Dundee
(Scotland). It is manufactured using the SEU hardened cell library from Atmel MH1RT CMOS
0.35µm radiation hardened sea of gates technology.
For any technical question relative to the functionality of the AT7910E please contact Atmel tech-
nical support at assp-applab.hotline@nto.atmel.com.
This document must be read in conjunction with the University of Dundee “SpaceWire Router
SpW-10X User Manual” available at www.atmel.com.
The SpaceWire router comprises the following functional logic blocks:
• Eight SpaceWire bi-directional serial ports.
• Two external parallel input/output ports each comprising an input FIFO and an output FIFO.
• A non-blocking crossbar switch connecting any input port to any output port.
• An internal configuration port accessible via the crossbar switch from the external parallel
input/output port or the SpaceWire input/output ports.
• A routing table accessible via the configuration port which holds the logical address to output
port mapping.
• Control logic to control the operation of the switch, performing arbitration and group adaptive
routing.
• Control registers than can be written and read by the configuration port and which hold
control information e.g. link operating speed.
• An external time-code interface comprising tick_in, tick_out and current tick count value
• Internal status/error registers accessible via the configuration port
• External status/error signals
A block diagram of the routing switch is given in the following figure:
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AT7910E
Figure 1-1. SpaceWire Router Block Diagram
Control
Logic
Routing
Table
SpaceWire
Port 1
SpaceWire
Port 2
SpaceWire
Port 3
Status/Error
Registers
Status
Outputs
SpaceWire
Port 4
SpaceWire
Interfaces
SpaceWire
Port 5
SpaceWire
Port 6
SpaceWire
Port 7
SpaceWire
Port 8
Control
Registers
Non-blocking
Crossbar
Configuration
Port
Switch
External
Input FIFO
Input/Output
Output FIFO
External Port
External
Input/Output
Input FIFO
Time-Code
Inputs /
Outputs
Time-Code
Interface
Output FIFO
External Port
1.1
SpaceWire Ports
The SpaceWire router has eight bi-directional SpaceWire links each conformant to the
SpaceWire standard.
Each SpaceWire link is controlled by an associated link register and routing control logic. Pack-
ets received on SpaceWire links are routed by the routing control logic to the configuration port,
other SpaceWire link ports or the external FIFO ports depending on the packet address.
Packets with invalid addresses are discarded by the SpaceWire router. The SpaceWire link sta-
tus is recorded in the associated link register and error status is held by the router until cleared
by a configuration command.
1.2
External Ports
The SpaceWire router has two bi-directional parallel FIFO interfaces that can be used to connect
the router to an external host system. The external port FIFO is two data characters deep.
Each FIFO is written to or read from synchronously with the 30MHz system clock. An eight-bit
data interface and an extra control bit for end of packet markers are provided by each external
port FIFO. Packets received by the external port are routed by the routing control logic to the
configuration port, SpaceWire link ports or the other external port depending on the packet
address.
Packets with invalid addresses are discarded by the SpaceWire router.
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1.3
Configuration Port
The SpaceWire router has one configuration port which performs read and write operations to
internal router registers.
Packets are routed to the configuration port when a packet with a leading address byte equal to
zero is received. The Remote Memory Access Protocol (RMAP) is used to access the configura-
tion port.
If an invalid command packet is received then the error is flagged to an associated status regis-
ter and the packet is discarded.
1.4
Routing table
The SpaceWire router routing table is set by the router command packets to assign logical
addresses to physical destination ports on the router.
A group of destination ports can be set, in each routing table location, to enable group adaptive
routing. When a packet is received with a logical address the routing table is checked by the
routing control logic and the packet is routed to the destination port when the port is ready. Rout-
ing table locations are set to invalid at power on or at reset.
The routing table logical addresses can also be set to support high priority and header deletion.
High priority packets are routed before low priority packets and header deletion of logical
addresses can be used to support regional logical addressing.
An invalid routing address will cause the packet to be spilled by the control logic.
1.5
Routing control logic and crossbar
The routing control logic is responsible for arbitration of output ports, group adaptive routing and
the crossbar switching. Arbitration is performed when two or more source ports are requesting
to use the same destination port.
A priority based arbitration scheme with two priority levels, high and low, is used where high pri-
ority packets are routed before low priority packets. Fair arbitration is performed on packets
which have the same priority levels to ensure each packet gets equal access to the output port.
Group adaptive routing control selects one of a number of output ports for sending out the
source packet.
1.6
Time Code Processing
An internal time-code register is used in the router to allow the router to be a time-code master
or a time-code slave.
In master mode the time-code interface is used to provide a tick-in to the SpaceWire routing
causing time-codes to be propagated through the network. Two modes of time master operation
are supported, an automatic mode where a time-code is propagated on each external tick-in and
a normal mode where the time-code is propagated dependent on the external time-in signal.
In time-code slave mode a valid received time-code, one plus the value of the router time-code
register, causes a tick-out to be sent to the SpaceWire links and the external time-code inter-
face. The time-code is propagated to all time-code ports except the port on which the time-code
was received. If the time-code received is not one plus the value of the time-code register then
the time-code register is updated but the tick-out is not performed.
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AT7910E
1.7
Control/Status Registers
The control and status registers in the SpaceWire router provide the means to control the opera-
tion of the router, set the router configuration and parameters or monitor the status of the device.
The registers are accessed using RMAP command packets received by the configuration port.
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2. Pin Configuration
Table 1. Pin assignment
Pin
Pin
Pin
Pin
Pin
Name
Name
Name
Name
Name
Number
Number
Number
Number
Number
1
VDDB
CLK
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
VSSB
VSSA
81
82
SIN-7
SOUT-7
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
EXTINDATA9_6
EXTINDATA9_7
EXTINDATA9_8
EXTINFULL9
VSSB
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
EXTTIMEIN2
EXTTIMEIN3
EXTTIMEIN4
EXTTIMEIN5
EXTTIMEIN6
EXTTIMEIN7
SELEXTTIME
TIMECTRRST
EXTTICKOUT
EXTTIMEOUT0
EXTTIMEOUT1
EXTTIMEOUT2
EXTTIMEOUT3
VSSB
2
3
RST
VDDA
83
SOUT+7
4
TESTIOE
TESTE
FEEDBDIV0
VSSA
VDDB
84
VSSB
5
DOUT-3
DOUT+3
DIN+4
85
VDDB
6
86
DOUT-7
VDDB
7
87
DOUT+7
EXTINWRITE9
EXTOUTDATA10_0
EXTOUTDATA10_1
EXTOUTDATA10_2
EXTOUTDATA10_3
EXTOUTDATA10_4
EXTOUTDATA10_5
VSSB
8
VDDA
DIN-4
88
DIN+8
9
FEEDBDIV1
FEEDBDIV2
VSSB
LVDS_REF
SIN+4
89
DIN-8
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
90
SIN+8
SIN-4
91
VSSA
VDDPLL
VCOBias
LOOPFILTER
VSSPLL
VDDB
SOUT-4
SOUT+4
DOUT-4
DOUT+4
VSSA
92
VDDA
93
SIN-8
94
SOUT-8
95
SOUT+8
VDDB
VDDB
96
DOUT-8
EXTOUTDATA10_6
EXTOUTDATA10_7
EXTOUTDATA10_8
EXTOUTEMPTY10
VSSA
EXTTIMEOUT4
EXTTIMEOUT5
EXTTIMEOUT6
EXTTIMEOUT7
STATMUXADDR0
STATMUXADDR1
STATMUXADDR2
STATMUXADDR3
VSSB
DIN+1
VDDA
97
DOUT+8
DIN-1
VSSB
98
VSSB
SIN+1
VDDB
99
VDDB
SIN-1
DIN+5
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
EXTOUTDATA9_0
EXTOUTDATA9_1
EXTOUTDATA9_2
EXTOUTDATA9_3
EXTOUTDATA9_4
VSSA
SOUT-1
SOUT+1
DOUT-1
DOUT+1
DIN+2
DIN-5
VDDA
SIN+5
EXTOUTREAD10
EXTINDATA10_0
EXTINDATA10_1
EXTINDATA10_2
EXTINDATA10_3
EXTINDATA10_4
EXTINDATA10_5
EXTINDATA10_6
EXTINDATA10_7
EXTINDATA10_8
EXTINFULL10
EXTINWRITE10
VSSA
SIN-5
SOUT-5
SOUT+5
DOUT-5
DOUT+5
DIN+6
VDDB
DIN-2
VDDA
STATMUXOUT0
STATMUXOUT1
STATMUXOUT2
VSSA
SIN+2
EXTOUTDATA9_5
VSSB
SIN-2
VSSB
DIN-6
VDDB
VDDB
SIN+6
EXTOUTDATA9_6
EXTOUTDATA9_7
EXTOUTDATA9_8
EXTOUTEMPTY9
EXTOUTREAD9
EXTINDATA9_0
EXTINDATA9_1
EXTINDATA9_2
EXTINDATA9_3
EXTINDATA9_4
EXTINDATA9_5
VDDA
SOUT-2
SOUT+2
DOUT-2
DOUT+2
DIN+3
SIN-6
STATMUXOUT3
STATMUXOUT4
STATMUXOUT5
STATMUXOUT6
STATMUXOUT7
VSSB
VSSB
VDDB
SOUT-6
SOUT+6
DOUT-6
DOUT+6
DIN+7
VDDA
DIN-3
VSSB
SIN+3
VDDB
SIN-3
EXTTICKIN
SOUT-3
SOUT+3
DIN-7
EXTTIMEIN0
SIN+7
EXTTIMEIN1
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AT7910E
3. Pin Description
Table 2. Pin description
Signal Name(1)(3)
Type(2)
Function
Buffer type
POWER
VDDA
VDDB
3.3V Power for the device
Ground for the device
VDDPLL
VSSA
VSSB
POWER
POWER
VSSPLL
LVDSRef
VCOBias
LoopFilter
LVDS Power reference for the device
Bias for the PLL VCO (Rvco)
Internal PLL filter
System Clock - Provides the reference clock for all the AT7910E modules
except the SpaceWire interface receivers
CLK
I
CMOS3V3
RST
I
I
Asynchronous active low system reset
CMOS3V3
CMOS3V3
FEEDBDIV[2:0]
PLL feedback divider configuration - Set the internal PLL output clock rate
DOUT+[1:8]
DOUT-[1:8]
O
O
I
LVDS+ LVDS-
LVDS+ LVDS-
LVDS+ LVDS-
LVDS+ LVDS-
Differential output pair - Data part of Data-Strobe SpaceWire link 1 to 8.
Differential output pair - Strobe part of Data-Strobe SpaceWire link 1 to 8.
Differential input pair - Data part of Data-Strobe SpaceWire link 1 to 8.
Differential input pair - Strobe part of Data-Strobe SpaceWire link 1 to 8.
SOUT+[1:8]
SOUT-[1:8]
DIN+[1:8]
DIN-[1:8]
SIN+[1:8]
SIN-[1:8]
I
Output data from external port zero FIFO.
Bit eight determines the data type data, EOP or EEP
EXTOUTDATA9[8:0]
EXTINDATA9[8:0]
O
I
CMOS3V3
CMOS3V3
Input data from external port zero FIFO.
Bit eight determines the data type data, EOP or EEP
FIFO ready signal for external output port zero. When high the FIFO has
data. When low the FIFO is empty
EXTOUTEMPTY9
EXTOUTREAD9
EXTINFULL9
O
I
CMOS3V3
CMOS3V3
CMOS3V3
CMOS3V3
CMOS3V3
Asserted Low to read from the external output port zero FIFO.
FIFO ready signal for external input port zero. When high there is space in
the FIFO so it can be written to. When low the FIFO is full.
O
I
EXTINWRITE9
Asserted Low to write to the external input port zero FIFO.
Output data from external port one FIFO.
Bit eight determines the data type data, EOP or EEP
EXTOUTDATA10[8:0]
O
Input data from external port one FIFO.
Bit eight determines the data type data, EOP or EEP
EXTINDATA10[8:0]
EXTOUTEMPTY10
I
CMOS3V3
CMOS3V3
FIFO ready signal for external output port one. When high the FIFO has
data. When low the FIFO is empty
O
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Signal Name(1)(3)
EXTOUTREAD10
Type(2)
I
Function
Buffer type
CMOS3V3
Asserted Low to read from the external output port one FIFO.
FIFO ready signal for external input port one. When high there is space in
the FIFO so it can be written to. When low the FIFO is full.
EXTINFULL10
O
I
CMOS3V3
CMOS3V3
EXTINWRITE10
Asserted Low to write to the external input port one FIFO.
The rising edge of the EXT_TICK_IN signal is used to indicate when a time-
code is to be sent
EXTTICKIN
I
I
CMOS3V3
CMOS3V3
EXT_TIME_IN(7:0) provides the value of the time-code to be distributed by
the router
EXTTIMEIN[7:0]
If SEL_EXT_TIME is high on the rising edge of EXT_TICK_IN the value on
EXT_TIME_IN(7:0) is loaded into the internal time-code register and
propagated by the router.
SELEXTTIME
I
CMOS3V3
TIMECTRRST
EXTTICKOUT
I
This signal causes the internal time-code counter to be reset to zero.
CMOS3V3
CMOS3V3
CMOS3V3
The falling edge of EXT_TICK_OUT is used to indicated the reception of a
time-code.
O
O
EXTTIMEOUT[7:0]
Received time-code value which is valid when EXT_TICK_OUT is asserted.
STATMUXADDR[3:0]
STATMUXOUT[7:0]
I
Select the error indication status signals to be output on STAT_MUX_OUT
CMOS3V3
CMOS3V3
After reset the STAT_MUX_OUT pins are inputs which define the power on
configuration status of the router.
I/O
After the power on reset configuration of the router has been read from
STAT_MUX_OUT the pins are driven as outputs by the router.
TESTEN
I
I
Shall be tied to ground
Shall be tied to ground
CMOS3V3
CMOS3V3
TESTIOEN
Notes: 1. Groups of pins represent busses where the highest number is the MSB.
2. O = Output; I = Input; I/O = Input/Output
3. XXX = active low signal
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AT7910E
4. Interfaces
The AT7910E provides a routing capability between eight SpaceWire links according to the
SpaceWire Standard ECSS-E-50-12A. In addition for use as a node interface, the AT7910E
integrates other interfaces such as:
• External ports
• Configuration port
• Time-code interface
• Control/Status interface
4.1
Spacewire ports
The SpaceWire router has eight bi-directional SpaceWire links each compliant with the
SpaceWire standard ECSS-E-50-12A.
Each SpaceWire link is controlled by an associated link register and routing control logic. Net-
work level error recovery is performed when an error is detected on the SpaceWire link as
defined in the SpaceWire standard. Packets received on SpaceWire links are routed by the
routing control logic to the configuration port, other SpaceWire link ports or the external FIFO
ports.
Packets with invalid addresses are discarded by the SpaceWire router dependent on the packet
address. The SpaceWire link status is recorded in the associated link register and error status is
held by the router until cleared by a configuration command.
4.2
External ports
The SpaceWire router has two bi-directional parallel FIFO interfaces to an external host system.
Each FIFO is written to or read from synchronously to the 30MHz system clock. An eight-bit
data interface and an extra control bit for end of packet markers are provided by each external
port FIFO.
Packets received by the external port are routed by the routing control logic to the configuration
port, SpaceWire link ports or the other external port dependent on the packet address.
Packets with invalid addresses are discarded by the SpaceWire router.
4.3
Configuration port
The SpaceWire router has one configuration port which performs read and write operations to
internal router registers. Packets are routed to the configuration port when a packet with a lead-
ing address byte of zero is received.
The SpaceWire Router supports the Remote Memory Access Protocol (RMAP) as command
packet format.
If an invalid command packet is received then the error is flagged to the associated status regis-
ter and the packet is discarded.
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4.4
Time-code interface
An internal time-code register is used in the router to allow the router to be a time-code master
or a time-code slave.
In master mode the time-code interface is used to provide a tick-in to the SpaceWire routing
causing time-codes to be propagated through the network. Two modes of time master operation
are supported, an automatic mode where a time-code is propagated on each external tick-in and
a normal mode where the time-code is propagated dependent on the external time-in signal.
In time-code slave mode a valid received time-code, one plus the value of the router time-code
register, causes a tick-out to be sent to the SpaceWire links and the external time-code inter-
face. The time-code is propagated to all time-code ports except the port on which the time-code
was received. If the time-code received is not one plus the value of the time-code register then
the time-code register is updated but the tick-out is not performed. In this way, circular network
paths do not cause a constant stream of time-codes to be sent in a loop.
4.5
Control/Status interface
The control and status registers in the SpaceWire router provide the means to control the opera-
tion of the router, set the router configuration and parameters or monitor the status of the device.
The registers are accessed using RMAP commands packets received by the configuration port.
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AT7910E
5. Typical Applications
The AT7910E SpaceWire router is perfectly suited for development of applications requiring a
standalone router, a terminal node with SpaceWire interface or a mixed configuration of the two
previous ones.
5.1
Stand-alone router
The AT7910E SpaceWire Router may be used as a stand-alone router with up to eight
SpaceWire links connected to it. Configuration of the routing tables etc. may be done by sending
SpaceWire packets containing configuration commands to the router.
Figure 5-1. AT7910E as SpaceWire router
5.2
Node interface
The SpaceWire Router has two external ports which enable the device to be used as a node
interface. The equipment to be connected to the SpaceWire network is attached to one or both
external ports. One or more SpaceWire ports are used to provide the connection into the
SpaceWire network. Unused SpaceWire ports may be disabled and their outputs tri-stated to
save power. In this arrangement configuration of the routing tables and other parameters may
be done by sending configuration packets from the local host via an external port or from a
remote network manager via a SpaceWire port.
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Figure 5-2. AT7910E as SpaceWire node interface
5.3
Embedded router
The SpaceWire Router device can also be used to provide a node with an embedded router. In
this case the external ports are used to provide the local connections to the node and the
SpaceWire ports are used to make connections to other ports in the network.
Figure 5-3. AT7910E as Embedded Router
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AT7910E
6. PLL Filter
The AT7910E uses an internal PLL to provide the base transmit clock signal for the SpaceWire
interfaces. External components are required to implement the PLL loop filter and to provide a
bias for the PLL VCO.
Note that RVCO, C and C0 are all connected to a quiet common ground track.
Dedicated decoupling capacitors are also required for the PLL power supply.
Figure 6-1. PLL filter and decoupling capacitors
Table 6-1.
PLL filter recommended components
R
C
10kΩ ± 5%, ¼W
120pF, ± 5%
C0
3.3pF, ± 5%
RVCO
4.7kΩ for 100-150MHz operation
1.8kΩ for 150-200MHz operation
Table 6-2.
PLL decoupling capacitors
Cpll1
Cpll2
100nF, ± 5%
1µF, ± 5%
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7. Electrical Characteristics
7.1
Absolute Maximum Ratings
Table 7-1.
Absolute Maximum Ratings
Parameter
Symbol
Value
Unit
Supply Voltage
I/O Voltage
VCC
-0.5 to +4
V
-0.5 to VCC + 0.5
-55 to +125
175
V
Operating Temperature
Range (Ambient)
TA
TJ
°C
°C
°C
Junction Temperature
Storage Temperature
Range
Tstg
-65 to +150
Thermal resistance
Junction to case
RThJC
5
°C/W
Stresses above those listed may cause permanent damage to the device.
7.2
DC Electrical Characteristics
Table 7-2.
3.3V operating range DC Characteristics
Parameter
Operating Voltage
Symbol
VCC
VIH
Min.
3.0
Max.
3.6
Unit
Conditions
V
Input HIGH Voltage
2.0
V
V
V
V
Input LOW Voltage
VIL
0.8
0.4
Output HIGH Voltage
Output LOW Voltage
Output Short circuit current
VOH
VOL
IOS
2.4
IOL = 3, 6, 12mA / VCC = VCC(min)
IOH = 3, 6, 12mA / VCC = VCC(min)
23
13
mA
mA
VOUT = VCC
VOUT = GND
7.3
Power consumption
Maximum power consumption figures at Vcc = 3.6V are presented in the following table.
Table 7-3.
3.3V Power Consumption
Power consumption [W] 2
Operation Mode
ICCSB - Standby
1.3 - TBC
ICCOP1 - 200Mb/s on SpaceWire links
ICCOP1 - 100Mb/s on SpaceWire links
ICCOP1 - 10Mb/s on SpaceWire links
3.8 - TBC
1.9 - TBC
0.9 - TBC
Notes: 1. Dynamic power with all interfaces active including external ports.
2. If a SpW IF is not active (switched off) assume a reduction of the static and dynamic power by
5%.
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AT7910E
7.4
AC Electrical Characteristics
The following table gives the worst case timings measured by Atmel on the 3.0V to 3.6V operat-
ing range
Table 7-4.
3.3V operating range timings(1)
Parameter
Symbol
Min.
Max.
Unit
Propagation delay CLK Low to DOUT0 High
Propagation delay CLK Low to DOUT1 High
Propagation delay CLK Low to DOUT2 High
Propagation delay CLK Low to DOUT3 High
Propagation delay CLK Low to DOUT4 High
Propagation delay CLK Low to DOUT5 High
Propagation delay CLK Low to DOUT6 High
Propagation delay CLK Low to DOUT7 High
Propagation delay CLK Low to DOUT0 Low
Propagation delay CLK Low to DOUT1 Low
Propagation delay CLK Low to DOUT2 Low
Propagation delay CLK Low to DOUT3 Low
Propagation delay CLK Low to DOUT4 Low
Propagation delay CLK Low to DOUT5 Low
Propagation delay CLK Low to DOUT6 Low
Propagation delay CLK Low to DOUT7 Low
Propagation delay CLK Low to SOUT0 High
Propagation delay CLK Low to SOUT1 High
Propagation delay CLK Low to SOUT2 High
Propagation delay CLK Low to SOUT3 High
Propagation delay CLK Low to SOUT4 High
Propagation delay CLK Low to SOUT5 High
Propagation delay CLK Low to SOUT6 High
Propagation delay CLK Low to SOUT7 High
Propagation delay CLK Low to SOUT0 Low
Propagation delay CLK Low to SOUT1 Low
Propagation delay CLK Low to SOUT2 Low
Propagation delay CLK Low to SOUT3 Low
Propagation delay CLK Low to SOUT4 Low
Tp0
16
ns
Tp1
Tp2
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
16
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
ns
Tp3
Tp4
Tp5
Tp6
Tp7
Tp8
Tp9
Tp10
Tp11
Tp12
Tp13
Tp14
Tp15
Tp16
Tp17
Tp18
Tp19
Tp20
Tp21
Tp22
Tp23
Tp24
Tp25
Tp26
Tp27
Tp28
15
7796B–AERO–08/08
Parameter
Symbol
Min.
Max.
Unit
Propagation delay CLK Low to SOUT5 Low
Tp29
16
ns
Propagation delay CLK Low to SOUT6 Low
Propagation delay CLK Low to SOUT7 Low
Tp30
Tp31
16
16
ns
ns
Note:
1. The timing parameters presented in the above table are measured under production configu-
ration (PLL bypassed and test mode enabled). During normal operation (PLL active and test
mode disabled) the propagation delay is directly linked to the PLL . Then, the timing figures are
not applicable under application conditions.
For guaranteed timings refer to the “Switching Characteristics” section of the ‘SpW-10X
SpaceWire Router User Manual’.
16
AT7910E
7796B–AERO–08/08
AT7910E
8. Package Drawings
8.1
MQFPF196
Here is a presentation of the mechanical outline of the 196 pins Ceramic Quad Flat Pack
(CQFP 196) package used for the AT7910E.
Figure 8-1. MQFPF 196 package
17
7796B–AERO–08/08
9. Ordering Information
Part-number
Temperature Range
Package
Quality Flow
AT7910EKB-E
AT7910EKB-MQ
AT7910EKB-SV
25°C
MQFPF196
Engineering sample
-55°C to +125°C
-55°C to +125°C
MQFPF196
MQFPF196
Mil Level B (*)
Space Level B (*)
(*) according to Atmel Quality flow document 4288, see Atmel web site.
10. Document Revision History
10.1 7796 Rev. B.
1. Corrected pinout error: pin 190 is VDDA and not VSSB. See Table 1 on page 6.
18
AT7910E
7796B–AERO–08/08
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