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Da Vinci Firmware 1
Firmware for the DaVinci-M rocket avionics board.
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Manages the rocket's flight phase from calibration to touchdown. More...

Data Structures | |
| struct | linear_acceleration_t |
| Represents a 3-axis linear acceleration vector from an IMU. More... | |
| struct | estimation_output_t |
| Holds the primary outputs of the state estimation filter (e.g., Kalman filter). More... | |
| struct | flight_fsm_t |
| Main data structure for the Flight State Machine. More... | |
Enumerations | |
| enum | flight_phase_t { INVALID , CALIBRATING , LIFTOFF , BURNING , ABCSDEPLOYED , DROGUE , MAIN , TOUCHDOWN } |
| Enumeration of all possible flight phases (states) in the FSM. More... | |
Manages the rocket's flight phase from calibration to touchdown.
| enum flight_phase_t |
Enumeration of all possible flight phases (states) in the FSM.
Definition at line 33 of file flight_control.h.