A Missile Autopilot Based on Feedback Linearization

Author:

Devaud Emmanuel,Siguerdidjane Houria

Publisher

Elsevier BV

Subject

General Engineering

Reference17 articles.

1. Commande optimale;Alexéev,1982

2. Approximate output tracking for nonlinear non-minimum phase system with an application to flight control;Benvenuti;Int J Robust Nonlinear Control,1994

3. Three-axes missile autopilot design from linear to nonlinear control strategies;Devaud;AIAA J Guidance, Control, Dynamics,2000

4. Some control strategies of a high angle of attack missile autopilot;Devaud;Control Eng Practice,2000

5. Optimisation approchee en boucle fermee des systemes non lineaires par la methodologie des perturbations singulieres;Fossard,1993

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