TY - GEN
T1 - Integrated design of missile guidance and control
T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
AU - Ran, Maopeng
AU - Chen, Yifen
AU - Wang, Qing
AU - Dong, Chaoyang
AU - Ma, Aojia
N1 - Publisher Copyright:
© 2014 IEEE.
PY - 2015/1/12
Y1 - 2015/1/12
N2 - 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.
AB - 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.
UR - https://www.scopus.com/pages/publications/84922567533
U2 - 10.1109/CGNCC.2014.7007226
DO - 10.1109/CGNCC.2014.7007226
M3 - 会议稿件
AN - SCOPUS:84922567533
T3 - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
SP - 115
EP - 119
BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
PB - Institute of Electrical and Electronics Engineers Inc.
Y2 - 8 August 2014 through 10 August 2014
ER -