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Da Vinci Firmware 1
Firmware for the DaVinci-M rocket avionics board.
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Defines the primary thresholds for detecting flight events. More...
Macros | |
| #define | LIFT_OFF_ACC_THRESHOLD 1.5f |
| Minimum vertical acceleration (in Gs) to trigger liftoff state. | |
| #define | END_OF_IGNITION_PHASE -0.5f |
| Vertical acceleration (in Gs) indicating motor burnout. | |
| #define | VELOCITY_BOUND_TOUCHDOWN 3.0F |
| Maximum vertical velocity (m/s) below which touchdown is considered possible. | |
| #define | MAIN_DEPLOY_HEIGHT 450 |
| Altitude in meters (m) for main parachute deployment. | |
Defines the primary thresholds for detecting flight events.
| #define END_OF_IGNITION_PHASE -0.5f |
Vertical acceleration (in Gs) indicating motor burnout.
Definition at line 48 of file FLIGHT_PARAMETERS_CONFIG.h.
| #define LIFT_OFF_ACC_THRESHOLD 1.5f |
Minimum vertical acceleration (in Gs) to trigger liftoff state.
Definition at line 47 of file FLIGHT_PARAMETERS_CONFIG.h.
| #define MAIN_DEPLOY_HEIGHT 450 |
Altitude in meters (m) for main parachute deployment.
Definition at line 50 of file FLIGHT_PARAMETERS_CONFIG.h.
| #define VELOCITY_BOUND_TOUCHDOWN 3.0F |
Maximum vertical velocity (m/s) below which touchdown is considered possible.
Definition at line 49 of file FLIGHT_PARAMETERS_CONFIG.h.