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This is the parent page for all Project Phoenix Avionics parts.

 

 

 

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COMPONENT

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PART

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QTY

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COST

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CPU

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STM32H743ZI2

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1

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10.65

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Flash Chip

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W25Q128JVSIM

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1

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1.40

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Radio Chip

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CC1200

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2

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11.92

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LNA

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TBD

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~10

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PA

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TBD

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~10

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Barometer

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Honeywell SSC

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1

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~35

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IMU

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IAM20680

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1

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15.50

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Accelerometer

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TBD

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~15

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GPS Module

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TBD

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~25

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COMPONENT

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PART

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QTY

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COST

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Barometer

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Honeywell SSC

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1

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~35

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IMU

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IAM20680

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1

...

.

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Accelerometer

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TBD

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~15

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GPS Module

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TBD

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~25

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Passives

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various

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~20

 

 

 

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)

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Testing

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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)

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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