Distributed Control of Spinning Flexible Spacecraft-Reference-Cited by-同舟云学术

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Distributed Control of Spinning Flexible Spacecraft

Published:1979-09 Issue:5 Volume:2 Page:407-415
ISSN:0162-3192
Container-title:Journal of Guidance and Control
language:en
Short-container-title:Journal of Guidance and Control

Author:

Meirovitch L.,VanLandingham H.F.,Oz H.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

General Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.55897

Reference13 articles.

1. 3Meirovitch, L., VanLandingham, H. F., and 6z, H. "Control of Spinning Flexible Spacecraft by Modal Synthesis,'* XXVII Congress, International Astronautical Federation, PaperIAF-76-022,Oct. 1976; also ActaAstronautica, Vol.4, 1977, pp.985-1010.

2. A theory of modal control

Cited by 16 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 model-free constrained control of postcapture flexible spacecraft: a Euler-Lagrange approach;J VIB CONTROL;2018

2. Variable structure slewing control and vibration damping of flexible spacecraft;Acta Astronautica;1991-01

3. Adaptive control of a two‐stage vibration isolation mount;The Journal of the Acoustical Society of America;1990-08

4. Rotational maneuver of nonlinear uncertain elastic spacecraft;IEEE Transactions on Aerospace and Electronic Systems;1988-03

5. Sensor/Actuator Selection and Placement for Control of Elastic Continua;IFAC Proceedings Volumes;1987-06

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