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Da Vinci Firmware 1
Firmware for the DaVinci-M rocket avionics board.
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Holds the primary outputs of the state estimation filter (e.g., Kalman filter). More...
#include <flight_control.h>
Data Fields | |
| float_t | height |
| Vertical altitude above ground level in meters (m). | |
| float_t | velocity |
| Vertical velocity in meters per second (m/s). | |
| float_t | acceleration |
| Vertical acceleration in meters per second squared (m/s^2). | |
Holds the primary outputs of the state estimation filter (e.g., Kalman filter).
Definition at line 58 of file flight_control.h.
| float_t estimation_output_t::acceleration |
Vertical acceleration in meters per second squared (m/s^2).
Definition at line 61 of file flight_control.h.
Referenced by StartFSM().
| float_t estimation_output_t::height |
Vertical altitude above ground level in meters (m).
Definition at line 59 of file flight_control.h.
Referenced by check_AbcsDeployed_phase(), check_Burning_phase(), check_Calibrating_phase(), check_Drogue_phase(), check_Liftoff_phase(), and StartFSM().
| float_t estimation_output_t::velocity |
Vertical velocity in meters per second (m/s).
Definition at line 60 of file flight_control.h.
Referenced by check_Main_phase(), and StartFSM().