In this chapter, a flight control system is designed for unmanned aerial vehicles (UAVs) based on the classical control methods. Separate discussions for controlling different parameters, such as altitude and heading, are given and controller design procedures are detailed. The explanations of design procedures are supported with Simulink diagrams, which will be helpful to the reader when designing their own controllers.
Classic Controller Design for Unmanned Aerial Vehicles
State Estimation and Control for Low-cost Unmanned Aerial Vehicles ; Kapitel : 9 ; 141-170
2015-01-01
30 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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