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.
Guidance and Control of Missile Interceptor using Second-Order Sliding Modes
IEEE Transactions on Aerospace and Electronic Systems ; 45 , 1 ; 110-124
2009-01-01
2002419 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Guidance and Control of Missile Interceptor using Second-Order Sliding Modes
Online Contents | 2009
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