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Disable failsafe until its actually tested
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754572f25a
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@ -234,15 +234,30 @@ mc_thread_main(int argc, char *argv[])
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}
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att_sp.thrust = manual.throttle;
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/* if the RC signal is lost, try to stay level and go slowly back down to ground */
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if(state.rc_signal_lost) {
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/* the failsafe throttle is stored as a parameter, as it depends on the copter and the payload */
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param_get(failsafe_throttle_handle, &failsafe_throttle);
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att_sp.roll_body = 0.0f;
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att_sp.pitch_body = 0.0f;
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att_sp.yaw_body = 0.0f;
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att_sp.thrust = failsafe_throttle;
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}
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// XXX disable this for now until its better checked
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// static bool rc_loss_first_time = true;
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// /* if the RC signal is lost, try to stay level and go slowly back down to ground */
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// if(state.rc_signal_lost) {
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// /* the failsafe throttle is stored as a parameter, as it depends on the copter and the payload */
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// param_get(failsafe_throttle_handle, &failsafe_throttle);
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// att_sp.roll_body = 0.0f;
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// att_sp.pitch_body = 0.0f;
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// /* keep current yaw, do not attempt to go to north orientation,
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// * since if the pilot regains RC control, he will be lost regarding
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// * the current orientation.
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// */
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// if (rc_loss_first_time)
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// att_sp.yaw_body = att.yaw;
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// // XXX hard-limit it to prevent ballistic mishaps - this is just supposed to
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// // slow a crash down, not actually keep the system in-air.
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// att_sp.thrust = (failsafe_throttle < 0.5f) : failsafe_throttle ? 0.5f;
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// rc_loss_first_time = false;
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// } else {
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// rc_loss_first_time = true;
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// }
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att_sp.timestamp = hrt_absolute_time();
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}
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