Assessment of the Feasibility of Intercepting an Intensively Maneuvering High-Speed Aircraft by an Inertial Interceptor with a Time-Varying Control Law

This paper presents a time-varying control law designed for an interceptor’s guidance to an intensively maneuvering aircraft (aerial target). The control law takes into account the mismatch between the dynamic properties of the interceptor and the target. Simulation results are provided, indicating the potential feasibility of intercepting the target and improving guidance accuracy.