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HIL fixed, fixedwing control fixes
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@@ -62,7 +62,7 @@ struct fixedwing_control_s
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float setpoint_rate_cast[3];
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float setpoint_attitude_rate[3];
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float setpoint_attitude[3];
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int16_t attitude_control_output[4]; /**< roll, pitch, yaw, throttle */
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float attitude_control_output[4]; /**< roll, pitch, yaw, throttle */
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float position_control_output[4];
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};
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