Title :
Integrated design of missile guidance and control: Active disturbance rejection control method
Author :
Maopeng Ran ; Yifen Chen ; Qing Wang ; Chaoyang Dong ; Aojia Ma
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
Abstract :
In this paper, we present an active disturbance rejection control (ADRC) based integrated guidance and control (IGC) law. The IGC law is designed using the backstepping technique, and the particle swarm optimization (PSO) algorithm is utilized to find the optimal selection of the controller parameters. Simulation results show that, with the application of the proposed IGC law, small miss distance can be achieved, and the system is robust against target maneuver and system uncertainties.
Keywords :
active disturbance rejection control; control nonlinearities; missile guidance; particle swarm optimisation; uncertain systems; ADRC; IGC law design; PSO algorithm; active disturbance rejection control method; backstepping technique; controller parameter selection; integrated design; integrated guidance and control; missile control; missile guidance; particle swarm optimization algorithm; system uncertainties; Aerodynamics; Backstepping; Educational institutions; History; Missiles; Observers; Uncertainty;
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.2014.7007226
