ATTITUDE CONTROL OF FLEXIBLE LAUNCH VEHICLE USING ADAPTIVE NOTCH FILTER-Reference-Cited by-同舟云学术

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ATTITUDE CONTROL OF FLEXIBLE LAUNCH VEHICLE USING ADAPTIVE NOTCH FILTER

Published:2005 Issue:1 Volume:38 Page:187-192
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Oh Choong-Seok,Bang Hyochoong

Publisher

Elsevier BV

Subject

General Medicine

Reference13 articles.

1. An Adaptive Control Approach to the Attitude Control of a Flexible Rocket;Choi;Control Engineering Practice, Aug.,2000

2. An Adaptive Tracking Filter for Bending-Mode Stabilization;Gaylor;AIAA Journal of Spacecraft and Rockets,1967

3. Analysis and Design of Space Vehicle Flight Control Systems;Greensite,1970

4. Control of Large Flexible Space Structures;Joshi,1989

5. The Finite Element Method using MATLAB;Kwon,2000

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. Elastic Adaptive Stability Control Technology of Launch Vehicle;Lecture Notes in Electrical Engineering;2023

2. On observability analysis and observer design for a class of nonlinear uncertain systems with general elastic vibration dynamics;Asian Journal of Control;2021-05-31

3. Attitude control of a flexible launch vehicle using an adaptive notch filter: Ground experiment;Control Engineering Practice;2008-01

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