forked from Archive/PX4-Autopilot
Bring fixed wing HIL back to normal mode, keep multicopter unchanged
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parent
2c2c4af599
commit
506c16f12a
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@ -763,9 +763,6 @@ private:
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MavlinkOrbSubscription *act_sub;
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struct actuator_outputs_s *act;
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MavlinkOrbSubscription *ctrl_sub;
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struct actuator_controls_s *ctrl;
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protected:
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void subscribe(Mavlink *mavlink)
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{
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@ -777,9 +774,6 @@ protected:
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act_sub = mavlink->add_orb_subscription(ORB_ID(actuator_outputs_0));
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act = (struct actuator_outputs_s *)act_sub->get_data();
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ctrl_sub = mavlink->add_orb_subscription(ORB_ID(actuator_controls_0));
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ctrl = (struct actuator_controls_s *)ctrl_sub->get_data();
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}
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void send(const hrt_abstime t)
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@ -787,7 +781,6 @@ protected:
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bool updated = status_sub->update(t);
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updated |= pos_sp_triplet_sub->update(t);
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updated |= act_sub->update(t);
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updated |= ctrl_sub->update(t);
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if (updated) {
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/* translate the current syste state to mavlink state and mode */
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@ -842,12 +835,30 @@ protected:
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0);
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} else {
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/* no special handling required, just send the controls */
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/* fixed wing: scale all channels except throttle -1 .. 1
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* because we know that we set the mixers up this way
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*/
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float out[8];
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const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2;
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for (unsigned i = 0; i < 8; i++) {
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if (i != 3) {
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/* scale fake PWM out 900..2100 us to -1..+1 for normal channels */
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out[i] = (act->output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2);
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} else {
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/* scale fake PWM out 900..2100 us to 0..1 for throttle */
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out[i] = (act->output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN);
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}
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}
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mavlink_msg_hil_controls_send(_channel,
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hrt_absolute_time(),
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ctrl->control[0], ctrl->control[1], ctrl->control[2], ctrl->control[3],
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ctrl->control[4], ctrl->control[5], ctrl->control[6], ctrl->control[7],
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out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
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mavlink_base_mode,
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0);
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}
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