Attitude Control of Satellites and Space Vehicles-Reference-Cited by-同舟云学术

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Attitude Control of Satellites and Space Vehicles

Published:1960 Issue: Volume: Page:351-436
ISSN:
Container-title:Advances in Space Science
language:
Short-container-title:

Author:

ROBERSON ROBERT E.

Publisher

Elsevier

Reference79 articles.

1. “L'Astronautique,”;Esnault-Pelterie,1930

2. A minimum orbital instrumented satellite—now;Singer;J. Brit. Interplanet. Soc.,1954

3. Control and power supply problems of instrumented satellites;Stuhlinger;Jet Propulsion,1956

4. Buchheim, R. W. (1956). Lunar instrument carrier—attitude stabilization. Rand Rept. RM-1730.

5. Stuhlinger, E. (1956). Instrumentation problems of unmanned satellites. Presented at the Semi-Annual Meeting American Rocket Society, Cleveland, June 1956; ARS Rept. 306–56.

Cited by 21 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. Hinged vehicle equations of motion;18th Aerospace Sciences Meeting;1980-01-14

2. On the dynamics of a system of rigid bodies;Theoretical and Applied Mechanics;1973

3. Time-optimal control of gravity-gradient satellites with disturbances;Journal of Spacecraft and Rockets;1970-12

4. State-space method for stability analysis of an attitude control system;Guidance, Control and Flight Mechanics Conference;1970-08-16

5. A linearization tool for use with matrix formalisms of rotational dynamics;Ingenieur-Archiv;1969

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