INVARIANT DESCRIPTION OF FIXED-WING UNMANNED AERIAL VEHICLE MOTION IN VERTICAL PLANE
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Abstract
This study presents an invariant description of fixed-wing unmanned aerial vehicle (UAV) motion within a vertical plane, yielding closed-form expressions for the invariants. Through integration specific to this UAV motion, invariants are determined as functions of the flight-path angle. The simulation results illustrate that the invariants remain unaffected by changes in heading angle, demonstrating consistent values regardless of heading direction. Additionally, the results show that an increase in bank angle correlates with a reduced rate of change in the invariants concerning flight-path angle. The obtained results offer insights into parameter evaluation and the development of invariant-based control and guidance methodologies.
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