This article considers the problem of trajectory tracking control for a micro fixed-wing unmanned air vehicle (UAV). With Bank-to-Turn (BTT) method to manage lateral deviation control of UAV, this paper discusses the outer loop guidance system, which separates the vehicle guidance problems into lateral control loop and longitudinal control loop. Based on the kinematic model of the coordinated turning of UAV, the aircraft can track a pre-specified flight path with desired error range. Flight test results on a fixed-wing UAV have indicated that the trajectory tracking control law is quite effective.
Trajectory Tracking Control for Micro Unmanned Aerial Vehicles
Advanced Materials Research ; 798-799 ; 448-451
2013-09-10
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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