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Table of Contents
Articles
| Preface |
PDF
|
| A. Tsourdos, H.Y. Chen, D. Alazard, B.A. White | 131-134 |
| Multi-objective Fuzzy Design of a Lateral Autopilot for a Quasi-Linear Parameter Varying Missile |
PDF
|
| Antonios Tsourdos, Evan J. Hughes, Brian A. White | 135-156 |
| An LFT approach to scheduled feedback design with an application to the synthesis of a missile autopilot |
PDF
|
| Y. Y. Le Gorrec, J.F. Magni | 157-172 |
| Computer-Aided Synthesis of Nonlinear Autopilots for Missiles |
PDF
|
| P.K. Menon, E.J. Ohlmeyer | 173-198 |
| Reduced order $H_\infty$ loop-shaping control of a missile pitch axis over a wide flight envelope |
PDF
|
| D. D. Farret, G. Duc, J.P. Harcaut | 199-214 |
| Missile Autopilot Design via Approximate Nonlinear Dynamic Inversion |
PDF
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| Antonios Tsourdos, Brian A. White | 215-226 |
| Model Following Control Approach for Missile Autopilot Design |
PDF
|
| Nabil Aouf, Henrique Mohallem Paiva, C.A. Rabbath, Marc Lauzon | 227-242 |
| Synthesis of missile gain-scheduled autopilots using an $H_\infty$-LPV technique with piecewise continuously differentiable parameter dependent Lyapunov functions |
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|
| P.C. Pellanda, A.M. Simoes, P. Apkarian, D. Alazard | 243-276 |
| 3D Nonlinear $H_2$/$H_1$ Guidance Law |
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| Hsin-Yuan Chen | 277-299 |