Adaptive, Integrated Guidance and Control Design for Automatic Landing of a fixed Wing UAV
are trained online with available measurements to compensate for inversion error due to unmodeled dynamics and modeling error of the aircraft in the design process. In addition, a reference command trajectory for the automatic landing control is designed in a way that the aircraft follows the lading pattern regardless of its initial position. The automatic landing system using IGC logic is evaluated using a sophisticated 6DOF nonlinear simulation program with the approach and landing scenario.
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