Analytical model of the rotation of an artificial satellite-Reference-Cited by-同舟云学术

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Analytical model of the rotation of an artificial satellite

Published:1990-07 Issue:4 Volume:13 Page:638-643
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Bois E.¹,Kovalevsky J.¹

Affiliation:

1. Observatoire de la Cote d'Azur, Grasse, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.25381

Reference15 articles.

1. Prospects for space stellar astrometry

2. Attitude Determination of the HIPPARCOS Satellite

3. First-order theory of satellite attitude motion application to HIPPARCOS

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. Semianalytical Technique for Six-Degree-of-Freedom Space Object Propagation;Journal of Guidance, Control, and Dynamics;2019-02

2. First-order accurate theory of perturbed circular motion;Celestial Mechanics & Dynamical Astronomy;1994-02

3. First Order Theory of Perturbed Circular Motion: An Application to Artificial Satellites;Predictability, Stability, and Chaos in N-Body Dynamical Systems;1991

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