A method of active attitude control based on energy considerations.
Author:
Affiliation:
1. Stanford University, Stanford, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29630
Reference5 articles.
1. Electric Propulsion/' Journal of Spacecraft and Rockets, Vol. 4, (9) No. 7, July 1967, pp. 852-858.
2. Moffit, T. P. and Klag, F. W. "Analytical Investigations of Cycle Characteristics for Advanced Turbo Electric Space Power Systems/' TN D-472, Oct. 1960, NASA.
3. Three-fourths t sub max rule for minimum-area space radiators
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