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FW stabalized mode properly initialize att_sp
This commit is contained in:
committed by
Lorenz Meier
parent
f3ec95c3b2
commit
41c1e56075
@@ -1063,13 +1063,17 @@ FixedwingAttitudeControl::task_main()
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* emit the manual setpoint here to allow attitude controller tuning
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* in attitude control mode.
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*/
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struct vehicle_attitude_setpoint_s att_sp;
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struct vehicle_attitude_setpoint_s att_sp = {};
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att_sp.timestamp = hrt_absolute_time();
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att_sp.roll_body = roll_sp;
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att_sp.pitch_body = pitch_sp;
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att_sp.yaw_body = 0.0f - _parameters.trim_yaw;
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att_sp.thrust = throttle_sp;
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att_sp.roll_reset_integral = false;
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att_sp.pitch_reset_integral = false;
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att_sp.yaw_reset_integral = false;
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/* lazily publish the setpoint only once available */
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if (_attitude_sp_pub != nullptr) {
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/* publish the attitude setpoint */
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@@ -2203,11 +2203,17 @@ Sensors::task_main()
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/* If the secondary failed as well, go to the tertiary, also only if available. */
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if (hrt_elapsed_time(&raw.gyro_timestamp[1]) > 20 * 1000 && _gyro_sub[2] >= 0) {
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fds[0].fd = _gyro_sub[2];
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warnx("failing over to third gyro");
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if (!_hil_enabled) {
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warnx("failing over to third gyro");
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}
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} else if (_gyro_sub[1] >= 0) {
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fds[0].fd = _gyro_sub[1];
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warnx("failing over to second gyro");
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if (!_hil_enabled) {
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warnx("failing over to second gyro");
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}
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}
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}
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