Robust Autopilot for a Quasi-Linear Parameter-Varying Missile Model

A sideslip velocity autopilot is designed for a model of a tactical missile, and robust stability of the closed-loop system is investigated. The tail-controlled missile in the cruciform fin configuration is modeled as a second-order quasi-linear parameter-varying system. This nonlinear model is obta...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2001-03, Vol.24 (2), p.287-295
Hauptverfasser:	Tsourdos, Antonios, Zbikowski, Rafal, White, Brian A
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engineering Applied sciences Automatic pilots Closed loop control systems Closed loop systems Computer science control theory systems Computer simulation Control system analysis Control system synthesis Control theory Control theory. Systems Controllers Design Equations of motion Equilibrium Exact sciences and technology Investigations Linear systems Linearization Mathematical models Missiles Parameter estimation Robust control Robustness (control systems) Sensors Simulation System stability Velocity
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