This is the parent page for all Project Phoenix Avionics.
Avionics Requirements:
Performance
MUST log telemetry locally in real time (5.1)
MUST confirm power on of system and adjacent components and state behaviour (5.2)
System MUST handle sensor failure gracefully (5.3)
system SHOULD estimate in the event of sensor failures (5.3.1)
System MUST ascertain the altitude/position of the rocket at high altitudes and speeds (5.4)
System MUST have the ability to estimate as well as Telemega (5.5)
Safety
Hardware no explosions protocol MUST be verifiable by firmware (5.9)
Software no explosions protocol MUST be implemented (5.10)
Testing
System MUST have full service hardware self-test/diagnostic (5.7)
All sensors
Radio
Flash
Daughter boards
Cameras
SHOULD include both sensor calibration and verification (5.7.8)
HOOTL testing capability currently a SHOULD (5.6)
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Integrated system MUST withstand vibration testing (9.1)
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Integrated system MUST have redundancy in pyros capabilities
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Integrated system MUST withstand supersonic flight
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Final integration procedure MUST be visually or electronically verifiable
Avionics information that isn't specific to project Pheonix is listed on the Avionics subteam's page. That includes information on DENNIS and how-to guides.
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