Control of a synchronous satellite by continuous radial thrust-Reference-Cited by-同舟云学术

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Control of a synchronous satellite by continuous radial thrust

Published:1964-07 Issue:7 Volume:2 Page:1179-1188
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

TOMS RONALD S. H.¹,KALENSHER B. E.¹

Affiliation:

1. Electro-Optical Systems, Inc., Pasadena, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2519

Reference10 articles.

1. October 1958;Levin E.

2. Citron, S. J. "Solutions for satellite motion under low acceleration using the method of variation of parameters/' ARS J. 31, 1786-1787(1961).

3. Dobrowolski, A. "Satellite orbit perturbations under a continuous radial thrust acceleration/' Jet Propulsion 28, 687-688 (1958).

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. Orbital perturbations and stationkeeping of communication satellites;Journal of Spacecraft and Rockets;1978-03

2. Design and Operational Aspects of All-Electric Thruster Control Systems for Geostationary Satellites;Journal of Spacecraft and Rockets;1975-11

3. All-Electric Thruster Control of a Geostationary Communications Satellite;Journal of Spacecraft and Rockets;1973-02

4. Flugeigenschaften geregelter drehsymmetrischer Flugkörper;Grundzüge der Flugmechanik und Ballistik;1969

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