takeoff_detect
Fixed-wing automatic launch detection When loaded, the pitch angle of plane is monitored, and will trigger the launch variable if the angle goes over a specified value (nose up) for 2 seconds. The launch variable can be reset to FALSE by pointing the nose to the ground. The module disables itself within a few seconds (4s) after detecting the launch. It can be re-actiaved by hand from the GCS.
None |
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|---|---|---|
Name |
Value |
Description |
TAKEOFF_DETECT_LAUNCH_PITCH |
30. |
Picth angle for takeoff detection (set ‘launch’ to TRUE) |
TAKEOFF_DETECT_ABORT_PITCH |
-20. |
Pitch angle to abort takeoff (set ‘launch’ to FALSE) |
TAKEOFF_DETECT_TIMER |
2. |
Timer for takeoff detection in seconds (default 2s above pitch angle threshold) |
TAKEOFF_DETECT_DISABLE_TIMER |
4. |
Timer for module de-activation (default 4s after the launch detection) |