TY - GEN
T1 - Design of the Cooperative Guidance Law with Simultaneous Constraints on Impact Time and Angle
AU - Zhou, Xing
AU - Yang, Baoqing
N1 - Publisher Copyright:
© 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
PY - 2023
Y1 - 2023
N2 - To address the problem of multiple missiles cooperatively intercepting a stationary target in three-dimensional (3D) space, a leader-following cooperative guidance law with constraints is proposed. Firstly, according to the 3D missiles-target relative motion equation, a 3D multi-missile cooperative guidance model is constructed. Secondly, based on the nonlinear dynamic inverse theory and time-scale separation, the control system is divided into slow-varying subsystems and fast-varying subsystems to simplify the design. Then, the cooperative guidance law is designed under the time constraints and the angle constraints, to ensure that the missiles can achieve time and space coordination within a limited time. Simulation case studies are carried out for the situation where one leader missile and three follower missiles are launched from different locations at the same time. The simulation results demonstrate the effectiveness of the cooperative guidance law. The practical importance of the design and the improvement direction of the design are finally summarized.
AB - To address the problem of multiple missiles cooperatively intercepting a stationary target in three-dimensional (3D) space, a leader-following cooperative guidance law with constraints is proposed. Firstly, according to the 3D missiles-target relative motion equation, a 3D multi-missile cooperative guidance model is constructed. Secondly, based on the nonlinear dynamic inverse theory and time-scale separation, the control system is divided into slow-varying subsystems and fast-varying subsystems to simplify the design. Then, the cooperative guidance law is designed under the time constraints and the angle constraints, to ensure that the missiles can achieve time and space coordination within a limited time. Simulation case studies are carried out for the situation where one leader missile and three follower missiles are launched from different locations at the same time. The simulation results demonstrate the effectiveness of the cooperative guidance law. The practical importance of the design and the improvement direction of the design are finally summarized.
KW - Angle constraint
KW - Cooperative guidance
KW - Leader-following
KW - Nonlinear dynamic inverse
KW - Time-scale separation
UR - https://www.scopus.com/pages/publications/85151150441
U2 - 10.1007/978-981-19-6613-2_507
DO - 10.1007/978-981-19-6613-2_507
M3 - 会议稿件
AN - SCOPUS:85151150441
SN - 9789811966125
T3 - Lecture Notes in Electrical Engineering
SP - 5250
EP - 5260
BT - Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
A2 - Yan, Liang
A2 - Duan, Haibin
A2 - Deng, Yimin
A2 - Yan, Liang
PB - Springer Science and Business Media Deutschland GmbH
T2 - International Conference on Guidance, Navigation and Control, ICGNC 2022
Y2 - 5 August 2022 through 7 August 2022
ER -