The proposed paper introduces the design of an adaptive augmentation of an Unmanned Aerial Vehicle's (UAV) Flight Control System (FCS). A Linear Quadratic Regulator (LQR) algorithm has been employed as a base-line control strategy and enhanced with an adaptation loop based on a Model Reference Adaptive Control (MRAC) technique.
Adaptive Augmentation of an Unmanned Aerial Vehicle's Flight Control System
01.09.2018
1472716 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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