TY - GEN
T1 - Research of Multi-Slide-Mode Non-singular Terminal Sliding Mode Guidance Law Based on Super Twisting Algorithm
AU - Chen, Wenxue
AU - Dong, Shiyin
AU - Fan, Yunfeng
AU - Liang, Xinru
AU - Gao, Changsheng
N1 - Publisher Copyright:
© 2022 Technical Committee on Control Theory, Chinese Association of Automation.
PY - 2022
Y1 - 2022
N2 - In this paper, Multi-Slide-Mode Non-singular Terminal Sliding Mode guidance law (MSMNTSMG) is designed based on the Super Twisting algorithm, and applied to intercept high-speed maneuvering targets in the near-space, which solves the singularity and chattering problems existing in traditional sliding mode interception guidance law. Firstly, the mathematical models and relative motion equations of missile and maneuvering target are established respectively. Based on the guidance equations, a new multi-slide-mode non-singular terminal sliding mode guidance law is designed, and the reaching law of Super Twisting algorithm is introduced. In the course of guidance law design, the acceleration of the maneuvering target is estimated adaptively and introduced into guidance instruction design to improve interception guidance effect. Finally, the simulation analysis proves that the multi-slide-mode non-singular terminal sliding mode guidance law based on super twisting algorithm can obviously improve the system singularity and chattering problems, and improve the convergence rate of the system compared with the traditional sliding mode guidance law.
AB - In this paper, Multi-Slide-Mode Non-singular Terminal Sliding Mode guidance law (MSMNTSMG) is designed based on the Super Twisting algorithm, and applied to intercept high-speed maneuvering targets in the near-space, which solves the singularity and chattering problems existing in traditional sliding mode interception guidance law. Firstly, the mathematical models and relative motion equations of missile and maneuvering target are established respectively. Based on the guidance equations, a new multi-slide-mode non-singular terminal sliding mode guidance law is designed, and the reaching law of Super Twisting algorithm is introduced. In the course of guidance law design, the acceleration of the maneuvering target is estimated adaptively and introduced into guidance instruction design to improve interception guidance effect. Finally, the simulation analysis proves that the multi-slide-mode non-singular terminal sliding mode guidance law based on super twisting algorithm can obviously improve the system singularity and chattering problems, and improve the convergence rate of the system compared with the traditional sliding mode guidance law.
KW - Interception guidance
KW - MSM
KW - Maneuvering target
KW - NTSMG
KW - Super Twisting algorithm
UR - https://www.scopus.com/pages/publications/85140448515
U2 - 10.23919/CCC55666.2022.9902361
DO - 10.23919/CCC55666.2022.9902361
M3 - 会议稿件
AN - SCOPUS:85140448515
T3 - Chinese Control Conference, CCC
SP - 3280
EP - 3286
BT - Proceedings of the 41st Chinese Control Conference, CCC 2022
A2 - Li, Zhijun
A2 - Sun, Jian
PB - IEEE Computer Society
T2 - 41st Chinese Control Conference, CCC 2022
Y2 - 25 July 2022 through 27 July 2022
ER -