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fw_att_control stabilized mode publish att_sp quat
This commit is contained in:
committed by
Andreas Daniel Antener
parent
12e5aca028
commit
9120082b0c
@@ -70,6 +70,9 @@
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#include <uORB/topics/vehicle_status.h>
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#include <uORB/uORB.h>
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using matrix::Eulerf;
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using matrix::Quatf;
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/**
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* Fixedwing attitude control app start / stop handling function
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*
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@@ -980,6 +983,14 @@ FixedwingAttitudeControl::task_main()
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_att_sp.pitch_body = math::constrain(_att_sp.pitch_body, -_parameters.man_pitch_max, _parameters.man_pitch_max);
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_att_sp.yaw_body = 0.0f;
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_att_sp.thrust = _manual.z;
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Quatf q(Eulerf(_att_sp.roll_body, _att_sp.pitch_body, _att_sp.yaw_body));
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_att_sp.q_d[0] = q(0);
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_att_sp.q_d[1] = q(1);
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_att_sp.q_d[2] = q(2);
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_att_sp.q_d[3] = q(3);
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_att_sp.q_d_valid = true;
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int instance;
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orb_publish_auto(_attitude_setpoint_id, &_attitude_sp_pub, &_att_sp, &instance, ORB_PRIO_DEFAULT);
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}
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