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Fixed zero offset in HIL
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@@ -447,25 +447,25 @@ l_actuator_outputs(struct listener *l)
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if (isfinite(act_outputs.output[3])
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if (isfinite(act_outputs.output[3])
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&& act_outputs.output[3] > 800 && act_outputs.output[3] < 2200) {
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&& act_outputs.output[3] > 800 && act_outputs.output[3] < 2200) {
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/* throttle is fourth output */
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/* throttle is fourth output */
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rudder = (act_outputs.output[2] - 1000.0f) / 1000.0f;
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rudder = (act_outputs.output[2] - 1500.0f) / 1000.0f;
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throttle = (act_outputs.output[3] - 1000.0f) / 1000.0f;
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throttle = (act_outputs.output[3] - 1500.0f) / 1000.0f;
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} else {
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} else {
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/* only three outputs, put throttle on position 4 / index 3 */
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/* only three outputs, put throttle on position 4 / index 3 */
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rudder = 0;
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rudder = 0;
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throttle = (act_outputs.output[2] - 1000.0f) / 1000.0f;
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throttle = (act_outputs.output[2] - 1500.0f) / 1000.0f;
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}
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}
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/* HIL message as per MAVLink spec */
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/* HIL message as per MAVLink spec */
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mavlink_msg_hil_controls_send(chan,
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mavlink_msg_hil_controls_send(chan,
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hrt_absolute_time(),
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hrt_absolute_time(),
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(act_outputs.output[0] - 1000.0f) / 1000.0f,
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(act_outputs.output[0] - 1500.0f) / 1000.0f,
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(act_outputs.output[1] - 1000.0f) / 1000.0f,
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(act_outputs.output[1] - 1500.0f) / 1000.0f,
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rudder,
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rudder,
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throttle,
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throttle,
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(act_outputs.output[4] - 1000.0f) / 1000.0f,
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(act_outputs.output[4] - 1500.0f) / 1000.0f,
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(act_outputs.output[5] - 1000.0f) / 1000.0f,
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(act_outputs.output[5] - 1500.0f) / 1000.0f,
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(act_outputs.output[6] - 1000.0f) / 1000.0f,
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(act_outputs.output[6] - 1500.0f) / 1000.0f,
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(act_outputs.output[7] - 1000.0f) / 1000.0f,
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(act_outputs.output[7] - 1500.0f) / 1000.0f,
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mavlink_mode,
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mavlink_mode,
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0);
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0);
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}
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}
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