TY - GEN
T1 - Command filtered adaptive control for integrated missile guidance and autopilot with terminal angular constraint
AU - Liang, Xiaoling
AU - Wang, Ning
AU - Liu, Yancheng
AU - Lv, Shuailin
AU - Xu, Bin
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/9/27
Y1 - 2016/9/27
N2 - For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.
AB - For homing missiles considering terminal angular constraint, integrated design of guidance and control utilizing adaptive command filtered backstepping is studied in this paper. The proposed control scheme guarantees not only the stability of the missile dynamics with state constraints but also the interception performance with a desired terminal attitude angle. An adaptive law is introduced to compensate unknown uncertainties in the varying-time system. Simulation results are further presented to show the effectiveness and performance of the proposed approach.
UR - http://www.scopus.com/inward/record.url?scp=84991699766&partnerID=8YFLogxK
U2 - 10.1109/WCICA.2016.7578525
DO - 10.1109/WCICA.2016.7578525
M3 - 会议稿件
AN - SCOPUS:84991699766
T3 - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
SP - 715
EP - 720
BT - Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 12th World Congress on Intelligent Control and Automation, WCICA 2016
Y2 - 12 June 2016 through 15 June 2016
ER -