I am currently configuring a flight termination system (FTS) that has to follow these rules:
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The FTS shall be automatically triggered:
• By breach of the Geo-fence.
• After 5 seconds of RC Signal loss. This is the connection directly between the
RC controller and the air vehicle.
• After no longer than 10 seconds from lost Datalink. -
The FTS shall not trigger a “return to home” action
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For fixed wing aircraft the following commands shall be set:
• Pitch: full nose up
• Roll: full right
• Yaw: full right -
The FTS shall also be triggered manually by the Flight Safety via the RC Controller.
Right now, I’m specifcally looking at the 4th point. Is this possible? I assume that a switch has to be configured so that the failsafe action is performed, but I am not sure how to do this. Right now, I believe I have the first three rules completed (it would be great if someone could look over them to see if they are also correct). I am currently using the advanced failsafe configuration, as the rules are similar to the Outback Challenge Competition: Advanced Failsafe Configuration — Plane documentation.
This is what I have configured until now:
- AFS_ENABLE = 1.
- AFS_TERM_ACTION = 42. This sets all control surfaces to maximum, and throttle is disarmed to enter a spin that deliberately dives the aircraft into the ground.
These are the conditions that will activate the FTS, and how they have been implemented:
- Geofence is breached
- FENCE_AUTOENABLE = 3 (AutoEnableOnlyWhenArmed
- The geofence becomes automatically active after arming the aircraft.
- FENCE_ALT_MAX sets the maximum altitude limit for the geofence (in metres). This is set to 200ft Above Ground Level (AGL) or 60.96m.
- FENCE_MARGIN is an Extra margin (in meters) outside the geofence before the action resulting from a geofence breach is triggered. This is set to its minimum as 1m.
- FENCE_ACTION?
The AFS will automatically search for a geofence breach and activate AFS_TERM_ACTION = 42.
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After 5s of RC signal loss
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THR_FS_VALUE = 1 enables RC Failsafe.
-
AFS_RC_FAIL_TIME = 5000 activates FTS after 5000ms or 5s of RC signal loss.
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After 10s of datalink loss
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FS_GCS_ENABLE = 1 enables GCS Failsafe
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AFS_GCS_TIMEOUT = 10 (default) defines how many seconds ardupilot will wait after the last MAVLink heartbeat before activating the FTS.
There is an option to terminate manually by setting AFS_TERMINATE = 1, but this is done by changing the parameter to mission planner and not through the RC controller.