Pre-defined time convergent non-singular terminal sliding mode guidance law with impact angle constraint

Yuxiang He, Fengyu Guo, Hao Zhang, Songlin Chen, Control and Simulation Center, Harbin Institute of Technology, School of Astronautics, National Key Laboratory of Modeling and Simulation for Complex Systems, Harbin Institute of Technology, Beijing Institute of Astronautical Systems Engineering, China Academy of Launch Vehicle Technology

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on July 24, 2025

Abstract

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
Compared to single missile intercepting a maneuvering target, multi-missile cooperative attack often has a better attack effect. But at the same time, it puts forward more stringent performance indicators for guidance law, requiring multiple missiles to ...