TY - JOUR
T1 - Spatio-temporal cooperative guidance law with switching topologies against unknown maneuvering target
T2 - A gain-tunable prescribed-time method
AU - Qin, Mingxing
AU - Xi, Jianxiang
AU - Wang, Le
AU - Wang, Cheng
AU - Zhao, Liangyu
N1 - Publisher Copyright:
© IMechE 2026
PY - 2026
Y1 - 2026
N2 - For the problem of multiple missiles attacking an unknown maneuvering target, this paper proposes a spatio-temporal cooperative guidance law, whose convergence time can be specified freely regardless of the initial states based on a gain-tunable prescribed-time stability criterion. This criterion not only enables switching between the time-invariant gain predefined-time stability method and the time-varying gain prescribed-time stability method by tuning the gain, but also eliminates the infinite gain issue of the latter without compromising the error convergence performance. Firstly, without requiring a priori knowledge of the maneuvering target, prescribed-time disturbance observers are constructed to guarantee prescribed-time convergence of the estimation errors on target acceleration components. Secondly, a distributed temporal cooperative guidance law is designed to achieve prescribed-time consensus on impact times of multiple missiles with switching topologies. Thirdly, a nonsingular sliding mode surface is presented to develop a spatial cooperative guidance law, enabling the line-of-sight angle of each missile to converge to a predetermined neighborhood around the desired value within a prescribed time. Finally, the effectiveness of the guidance law and its robustness against communication topology switching are verified through simulations.
AB - For the problem of multiple missiles attacking an unknown maneuvering target, this paper proposes a spatio-temporal cooperative guidance law, whose convergence time can be specified freely regardless of the initial states based on a gain-tunable prescribed-time stability criterion. This criterion not only enables switching between the time-invariant gain predefined-time stability method and the time-varying gain prescribed-time stability method by tuning the gain, but also eliminates the infinite gain issue of the latter without compromising the error convergence performance. Firstly, without requiring a priori knowledge of the maneuvering target, prescribed-time disturbance observers are constructed to guarantee prescribed-time convergence of the estimation errors on target acceleration components. Secondly, a distributed temporal cooperative guidance law is designed to achieve prescribed-time consensus on impact times of multiple missiles with switching topologies. Thirdly, a nonsingular sliding mode surface is presented to develop a spatial cooperative guidance law, enabling the line-of-sight angle of each missile to converge to a predetermined neighborhood around the desired value within a prescribed time. Finally, the effectiveness of the guidance law and its robustness against communication topology switching are verified through simulations.
KW - cooperative guidance
KW - gain-tunable approach
KW - impact angle constraints
KW - prescribed-time convergence
KW - switching communication topologies
KW - time consensus
UR - https://www.scopus.com/pages/publications/105041023868
U2 - 10.1177/09544100261451552
DO - 10.1177/09544100261451552
M3 - Article
AN - SCOPUS:105041023868
SN - 0954-4100
JO - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
JF - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
ER -