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Guidance and Control of Missile Interceptor using Second-Order Sliding Modes

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3 Author(s)
Yuri B. Shtessel ; The University of Alabama in Huntsville ; Ilya A. Shkolnikov ; Arie Levant

A new smooth second-order sliding mode control (SSOSM) is proposed and proved for a system driven by uncertain sufficiently smooth disturbances. The main target application of this technique, the missile interceptor guidance-control system against targets performing evasive maneuvers, is considered to demonstrate benefits of this design for a two-loop integration of guidance and flight control systems. The designed guidance-control system performance is verified via computer simulations using a miniature hypervelocity kinetic energy endo-atmospheric interceptor planar model.

Published in:

IEEE Transactions on Aerospace and Electronic Systems  (Volume:45 ,  Issue: 1 )