Missile autopilot design via a modified LPV synthesis technique-Reference-Cited by-同舟云学术

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Missile autopilot design via a modified LPV synthesis technique

Published:1999-04 Issue:3 Volume:3 Page:153-160
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Biannic J.-M.,Apkarian P.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference15 articles.

1. Self-scheduled H∞ control of missile via linear matrix inequalities;Apkarian;J. Guid. Control Dynam.,1995

2. A convex characterization of gain-scheduled H∞ Controllers;Apkarian;IEEE T. Automat. Contr.,1995

3. Design of robust time-varying controllers for missile autopilot;Balas,1992

4. Parameter-dependent control of an under-actuated mechanical system;Becker,1995

5. Control of parametrically-dependent linear systems: A single quadratic Lyapunov approach;Becker,1993

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2. Missile Autopilot Design via Structured Robust Linear Parameter-Varying Synthesis;Journal of Guidance, Control, and Dynamics;2023-08

3. Uneven Grid-based Linear Parameter-Varying Controller Design for Guided Projectiles;IFAC-PapersOnLine;2023

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