Marsaut_0 experimental rocket avionic (On-board electronics) created by Mines Space, Version 2021 launched at C'space
CC BY-NC-SA 4.0
The electronic architecture of our rocket is divided into two parts, the flight controller (Sequencer) and the payload. You can find the CAD of all the cards on this link : https://grabcad.com/library/avionics-system-for-marsaut-0-rocket-mines-space-1
- Branch APU : The APU (Acquisition Process Unit) board is dedicated to the acquisition,
storage and transmission of data in the rocket.
- Branch SEQ : The SEQ board (the flight controller) is dedicated to the control of the different
actuators according to the rocket's flight status.
- Branch ALIM : The ALIM board (the power supply board) is the board in charge of the electrical
distribution and the control of the battery status.
- Branch MOTOR : The MOTOR board is equipped with motor drivers for parachute deployment control.
- Branch IHM : The HMI card is the card dedicated to the control and restitution
of information to the user.
- Branch INT_LTS : The INT_LTS card is an interface card with the Lora TTGO-T BEAM card.
- Branch LINK : The LINK card allows to link all the actuators and sensors
installed in the rocket to the electronics .
