An active nutation control system for spin stabilised satellites-Reference-Cited by-同舟云学术

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An active nutation control system for spin stabilised satellites

Published:1977-03 Issue:2 Volume:13 Page:161-172
ISSN:0005-1098
Container-title:Automatica
language:en
Short-container-title:Automatica

Author:

Devey W.J.,Field C.F.,Flook L.

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Control and Systems Engineering

Reference6 articles.

1. An on-board closed loop nutation control system for a spin stabilised spacecraft;Grasshoff;J. Spacecraft Rocket,1968

2. Flight test of a pitch control for a spinning vehicle;Garner;TN D-1922, N.A.S.A,1963

3. 4th Communications Satellite Systems Conf;Neer,1972

4. An active nutation control system for spin stabilised satellites;Devey,1973

5. J. T. Hrastor: Testing a satellite automatic nutation control system. NASA TN-D-7596.

Cited by 10 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. Active nutation control of an asymmetric spacecraft using an axial reaction wheel;Advances in Space Research;2016-12

2. Lyapunov-Based Control for Flat-Spin Recovery and Spin Inversion of Spin-Stabilized Spacecraft;AIAA/AAS Astrodynamics Specialist Conference;2016-09-09

3. Preliminary Design and Prototyping of a Low-Cost Spacecraft Attitude Determination and Control Setup;AIAA Guidance, Navigation, and Control Conference;2015-01-02

4. Study of Wheel Activated Gyroscopic-like Motion in Spacecraft Rotational Dynamics;Procedia Engineering;2013

5. Predictive Nutation and Spin Inversion Control of Spin-Stabilized Spacecraft;Journal of Spacecraft and Rockets;2010-11

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