Vol. 11 No. 2 (2004): Special Issue: Control of Defense Systems

Articles

• Preface

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• Multi-objective Fuzzy Design of a Lateral Autopilot for a Quasi-Linear Parameter Varying Missile

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• An LFT approach to scheduled feedback design with an application to the synthesis of a missile autopilot

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• Computer-Aided Synthesis of Nonlinear Autopilots for Missiles

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• Reduced order $H_\infty$ loop-shaping control of a missile pitch axis over a wide flight envelope

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• Missile Autopilot Design via Approximate Nonlinear Dynamic Inversion

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• Model Following Control Approach for Missile Autopilot Design

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• Synthesis of missile gain-scheduled autopilots using an $H_\infty$-LPV technique with piecewise continuously differentiable parameter dependent Lyapunov functions

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• 3D Nonlinear $H_2$/$H_1$ Guidance Law

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