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

fYear

2014

fDate

8-10 Aug. 2014

Firstpage

115

Lastpage

119

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese

Conference_Location

Yantai

Print_ISBN

978-1-4799-4700-3

Type

conf

DOI

10.1109/CGNCC.2014.7007226

Filename

7007226