Plane: clean up cm-to-m conversion in nav_control_output
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@ -177,12 +177,12 @@ void GCS_MAVLINK_Plane::send_nav_controller_output() const
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mavlink_msg_nav_controller_output_send(
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chan,
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targets.x * 1.0e-2f,
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targets.y * 1.0e-2f,
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targets.z * 1.0e-2f,
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targets.x * 0.01,
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targets.y * 0.01,
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targets.z * 0.01,
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wp_nav_valid ? quadplane.wp_nav->get_wp_bearing_to_destination() : 0,
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wp_nav_valid ? MIN(quadplane.wp_nav->get_wp_distance_to_destination() * 1.0e-2f, UINT16_MAX) : 0,
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(plane.control_mode != &plane.mode_qstabilize) ? quadplane.pos_control->get_pos_error_z_cm() * 1.0e-2f : 0,
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wp_nav_valid ? MIN(quadplane.wp_nav->get_wp_distance_to_destination() * 0.01, UINT16_MAX) : 0,
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(plane.control_mode != &plane.mode_qstabilize) ? quadplane.pos_control->get_pos_error_z_cm() * 0.01 : 0,
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plane.airspeed_error * 100,
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wp_nav_valid ? quadplane.wp_nav->crosstrack_error() : 0);
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return;
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@ -192,12 +192,12 @@ void GCS_MAVLINK_Plane::send_nav_controller_output() const
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const AP_Navigation *nav_controller = plane.nav_controller;
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mavlink_msg_nav_controller_output_send(
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chan,
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plane.nav_roll_cd * 0.01f,
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plane.nav_pitch_cd * 0.01f,
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nav_controller->nav_bearing_cd() * 0.01f,
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nav_controller->target_bearing_cd() * 0.01f,
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plane.nav_roll_cd * 0.01,
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plane.nav_pitch_cd * 0.01,
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nav_controller->nav_bearing_cd() * 0.01,
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nav_controller->target_bearing_cd() * 0.01,
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MIN(plane.auto_state.wp_distance, UINT16_MAX),
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plane.altitude_error_cm * 0.01f,
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plane.altitude_error_cm * 0.01,
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plane.airspeed_error * 100,
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nav_controller->crosstrack_error());
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}
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