Robust Impulse-to-Peak Synthesis: Application to the Control of an Aerospace Launcher-Reference-Cited by-同舟云学术

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Robust Impulse-to-Peak Synthesis: Application to the Control of an Aerospace Launcher

Published:2004-06 Issue:6 Volume:37 Page:967-972
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Arzelier D.,Peaucelle D.

Publisher

Elsevier BV

Subject

General Medicine

Reference12 articles.

1. Linear Matrix Inequalities in System and Control Theory;Boyd,1994

2. A multiobjective control algorithm: Application to a launcher with bending modes;Clement,2000

3. Acrospace launch vehicle control: A gain scheduing approach;Clement,2002

4. Extended H2 and H∞ norm characterizations and controller parametrizations for discrete-time systems;de Oliveira;International Journal of Control,2002

Cited by 3 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. A Linear Quadratic Integral Design Approach for the Automatic Control System of a Launch Vehicle;Applied Mechanics and Materials;2015-07

2. An H_∞ State Feedback Control Law for Launch Vehicles;Applied Mechanics and Materials;2014-10

3. Comparative analysis of architectures for the control loop of launch vehicles during atmospheric flight;Aerospace Science and Technology;2009-03

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