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Application of Two-Time Scale Method in Missile Autopilot Design

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Abstract (2. Language): 
In this paper two-time scale method is used to control an 8-DOF missile autopilot. The mathematical model is developed using the singular perturbation theory. Structural properties of the system in terms of the slow and fast subsystems are established. An asymptotically optimal two-time scale controller was developed for missile. The two-time scale controller was compared to the optimal controller, and it was demonstrated that there is negligible degradation in performance

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