Three-dimensional prescribed performance sliding mode guidance law for intercepting maneuvering target

Abstract

This article describes three-dimensional sliding mode guidance laws with prescribed performance. The proposed guidance laws can ensure that the line of sight (LOS) angle converges according to the prescribed performance, and the convergence rate, the steady-state error and the maximum overshoot can be preset in advance. By combining the LOS tracking error with the performance constraint function, a new error variable function is designed, and then the prescribed performance control problem is transformed into that of the boundedness of the error variable function. The key concept in this approach is to design a new sliding mode surface to ensure that the error variable function is bounded, so as to ensure that the system state converges according to the prescribed performance. Additionally, this article discusses the problem whereby the upper bound of the aggregate uncertainty, including the target information, is unavailable. An adaptive guidance law is presented for this scenario. Finally, simulations comparisons are conducted with other forms of guidance laws. Simulation results show that the guidance laws proposed in this article achieve effective performance.

Predefined-time prescribed performance guidance law design against maneuvering target under input saturation

“…The terminal guidance process is investigated in our work. In the line of sight (LOS) coordinate frame, the dynamic in [1], [7], and [9] between an interceptor and a target in 3D space is presented as: (…”