forked from Archive/PX4-Autopilot
mavlink: use all outputs in HIL mode
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5bb8c50112
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dca8daeec5
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@ -1051,10 +1051,16 @@ protected:
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uint32_t mavlink_custom_mode;
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get_mavlink_mode_state(&status, &pos_sp_triplet, &mavlink_state, &mavlink_base_mode, &mavlink_custom_mode);
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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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/* scale outputs depending on system type */
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if (mavlink_system.type == MAV_TYPE_QUADROTOR ||
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mavlink_system.type == MAV_TYPE_HEXAROTOR ||
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mavlink_system.type == MAV_TYPE_OCTOROTOR) {
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/* set number of valid outputs depending on vehicle type */
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/* multirotors: set number of rotor outputs depending on type */
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unsigned n;
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switch (mavlink_system.type) {
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@ -1071,59 +1077,44 @@ protected:
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break;
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}
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/* scale / assign outputs depending on system type */
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float out[8];
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for (unsigned i = 0; i < 8; i++) {
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if (i < n) {
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if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) {
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/* scale fake PWM out 900..2100 us to 0..1 for normal multirotors */
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if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) {
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if (i < n) {
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/* scale PWM out 900..2100 us to 0..1 for rotors */
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out[i] = (act.output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN);
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} else {
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/* send 0 when disarmed */
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out[i] = 0.0f;
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/* scale PWM out 900..2100 us to -1..1 for other channels */
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out[i] = (act.output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2);
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}
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} else {
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out[i] = -1.0f;
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/* send 0 when disarmed */
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out[i] = 0.0f;
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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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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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} else {
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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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/* fixed wing: scale throttle to 0..1 and other channels to -1..1 */
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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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/* scale 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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/* scale 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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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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mavlink_msg_hil_controls_send(_channel,
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hrt_absolute_time(),
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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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}
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};
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