APPENDIX AVI212 Especificações Página 35

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Gaia
GAIA.ASU.SP.ESM.00007
Issue 2.00
Page 35 of 79
Astrium Ltd owns the copyright of this document which is supplied in confidence and which shall not be used for any purpose other than that for which it is supplied and shall not in
whole or in part be reproduced, copied, or communicated to any person without written permission from the owner.
GAIA.ASU.SP.ESM.00007 (Avionics SCOE Req Iss 2).doc
3.6.5.2 CPS LV Status Simulation
AVI-346/CREATED/T
LV Status Simulation function shall be provided by relay simulation (18x) of each LV STATUS micro-
switch.
AVI-347/CREATED/T
LV Status Simulation shall conform to the following specifications: [AD06] Table 3.5-28 (Relay Status
Acquisition Source Specification).
AVI-348/CREATED/T
In open-loop test modes LV STATUS (OPEN/CLOSE) relay shall be set to the STATE value of the
corresponding LV command pulse acquisition (see AVI-382).
AVI-1609/CREATED/T
In open-loop test modes, it shall be possible to overwrite the LV STATUS from the local MMI or from
the CCS (Test Procedure/Command Line).
Note: This allows error injection into the EIU - Latch Valve Status not reflecting the commanded
operation.
AVI-1608/CREATED/T
In closed-loop test mode, LV STATUS shall be defined by the RTS.
3.6.5.3 CPS FCV Command Pulse Acquisition
AVI-359/EIU-713/T
The FCV Command Pulse Acquisition interface shall be provided by fixed loads (16x) simulating each
of the FCV coils.
AVI-360/EIU-715/T
The FCV Command Acquisition interface shall conform to the following specifications: [AD06] Table
3.5-36 (Flow Control Valve Interface Specification - Receiver Circuit Specification).
AVI-378/CREATED/T
FCV Command Pulse Acquisition shall provide measurements of the integrated ON time for each
FCV, the individual command pulse widths and an event count per FCV, as detailed below:
EVENT COUNT limit 65536
ON time resolution 5 %
Pulse WIDTH resolution
100.0 µs - for pulse widths 5ms to continuous
Table 3.6-3: CPS - FCV Command Pulse Measurement Specification
AVI-372/CREATED/T
Once an FCV Command has triggered, ON time measurements shall be integrated every 15.625 ms
(equivalent to the RTS Simulation Cycle rate of 1/64 of the Major Frame rate) and calculated as
percentage (ON) over the integration period. TBC
Note: Although the CPS Model in the RTS executes at 64Hz in real-time, thrust vectors output to the
Dynamics Model need to consider thruster pulses to an accuracy of <1ms.
AVI-1887/CREATED/T
Measurement of LV Command pulses shall be triggered asynchronously by detection of an incoming
pulse with the following specifications:
Pulse Width > 1ms
Pulse Amplitude > 10.0V
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