Modern Missile Flight Control Design: An Overview-Reference-Cited by-同舟云学术

Modern Missile Flight Control Design: An Overview

Published:2001-09 Issue:15 Volume:34 Page:425-430
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Tsourdos Antonios,White Brian A.

Publisher

Elsevier BV

Subject

General Medicine

Reference38 articles.

1. Self-scheduled H∞ control of missile via linear matrix inequalities;Apkarian;Journal of Guidance, Control and Dynamics,1995

2. Adaptive Control;Åstrom,1989

3. The μ-Analysis and Synthesis Toolbox;Balas,1994

4. On linear-quadratic adaptive control for the desin of missile autopilots;Bendotti;Optimal Control Applications & Methods,1993

5. Gain scheduled bank-to-turn autopilot design using linear parameter-varying transformations;Carter;Journal of Mathematical Analysis and Applications,1996

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Adaptive reinforcement learning control for a class of missiles with aerodynamic uncertainties and unmodeled dynamics;The Aeronautical Journal;2023-07-06

2. Linearized State-Space Model-Based Attitude Control for Rocket With Four Controllable Fins—Part 1-1: Basic Modeling and Identification;IEEE Access;2023

3. Adaptive Control of Aircraft Lateral Movement in Landing Mode11New algorithm for control of aircraft (Sec. 3) was developed under support of RNF (grant 14-29-00142) in IPME RAS. The other research were partially supported by grant of Russian Foundation for Basic Research N0 13-08-01014, 14-08-01015, Ministry of Education and Science of Russian Federation (Project 14.Z50.31.0031) and Government of Russian Federation, Grant 074-U01.;IFAC-PapersOnLine;2015

4. Robust Control of Aircraft Lateral Movement 1;IFAC Proceedings Volumes;2014

5. Passification-based robust flight control design;Automatica;2011-12