Attitude stability of flexible spacecraft which use dual time constant feedback lag network pseudorate control-Reference-Cited by-同舟云学术

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Attitude stability of flexible spacecraft which use dual time constant feedback lag network pseudorate control

Published:1976-04-05 Issue: Volume: Page:
ISSN:
Container-title:6th Communications Satellite Systems Conference
language:
Short-container-title:

Author:

MILLAR R.¹,VIGNERON F.¹

Affiliation:

1. Department of Communications, Communications Research Centre, Ottawa, Canada

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1976-266

Reference8 articles.

1. Creensite,A.L. &lL!jLand Design of Space Vehicle Fl.i.&t Control Systems,Control Theory: Volume 11, Spartan Rooks,1970,pp.305-316, 345.

Cited by 4 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. Fault-tolerant attitude control of the satellite in the presence of simultaneous actuator and sensor faults;Scientific Reports;2023-11-27

2. Vibration suppression of flexible spacecraft during attitude control;Acta Astronautica;2001-07

3. Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper;Guidance, Navigation, and Control Conference;1997-08-11

4. Design and simulation of state estimators for a 3-axis stabilized communications satellite;18th Aerospace Sciences Meeting;1980-01-14

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