Title :
Rapid turning maneuver flight control for a high agility UAV using robust adaptive augmented backstepping
Author :
Yi Yang ; Xin Chen ; Chuntao Li
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Abstract :
The paper presents a new robust adaptive augmented backstepping control scheme for rapid turning maneuver of a high agility unmanned aerial vehicle (UAV). The proposed control scheme consists of a baseline backstepping controller which can deal with the couplings of kinematic and inertial during fast rolling and generates commands tracking control inputs, and a robust adaptive compensator which can ensure bounded output tracking error in the presence of unmodeled dynamics. Effectiveness and robustness of the designed scheme has been verified through detailed stability analysis and a number of simulations on a nonlinear 6DOF UAV model which show that the proposed robust adaptive augmented controller is competent to perform rapid turning maneuver in full flight envelop and improve the robustness of flight control system substantially.
Keywords :
adaptive control; aerospace control; autonomous aerial vehicles; compensation; control nonlinearities; nonlinear control systems; position control; robot kinematics; robust control; vehicle dynamics; baseline backstepping controller; bounded output tracking error; commands tracking control input; flight control system; inertial coupling; kinematic coupling; nonlinear UAV model; rapid turning maneuver flight control; robust adaptive augmented backstepping control scheme; robust adaptive augmented controller; robust adaptive compensator; robustness; stability analysis; unmanned aerial vehicle; unmodeled dynamics; Aerodynamics; Backstepping; Equations; Robustness; Turning; Vectors; Vehicle dynamics;
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
DOI :
10.1109/CGNCC.2014.7007401