TY - GEN
T1 - Adding a power integrator technique based terminal guidance law
AU - Wang, Songyan
AU - Sun, Xiangyu
AU - Chao, Tao
AU - Ma, Ping
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - In this paper a novel terminal guidance law for hypersonic vehicle is investigated. In order to accelerate the convergence rate of line of sight angle, adding a power integrator technique based nonlinear guidance law which can make the line of sight converge to zero in finite time is proposed. Then rigorous stability analysis of finite-time convergence is shown. It demonstrates the effectiveness of the approach by numerical simulation meanwhile the approach have strong robustness in the presence of disturbance.
AB - In this paper a novel terminal guidance law for hypersonic vehicle is investigated. In order to accelerate the convergence rate of line of sight angle, adding a power integrator technique based nonlinear guidance law which can make the line of sight converge to zero in finite time is proposed. Then rigorous stability analysis of finite-time convergence is shown. It demonstrates the effectiveness of the approach by numerical simulation meanwhile the approach have strong robustness in the presence of disturbance.
UR - https://www.scopus.com/pages/publications/85015216966
U2 - 10.1109/CGNCC.2016.7829107
DO - 10.1109/CGNCC.2016.7829107
M3 - 会议稿件
AN - SCOPUS:85015216966
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 2053
EP - 2057
BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Y2 - 12 August 2016 through 14 August 2016
ER -