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added option for direct yaw control with rudder for fixed wing
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@@ -21,3 +21,5 @@ float32 thrust # Thrust in Newton the power system should generate
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bool roll_reset_integral # Reset roll integral part (navigation logic change)
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bool roll_reset_integral # Reset roll integral part (navigation logic change)
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bool pitch_reset_integral # Reset pitch integral part (navigation logic change)
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bool pitch_reset_integral # Reset pitch integral part (navigation logic change)
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bool yaw_reset_integral # Reset yaw integral part (navigation logic change)
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bool yaw_reset_integral # Reset yaw integral part (navigation logic change)
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bool fw_control_yaw # control heading with rudder (used for auto takeoff on runway)
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