Each of following flight phases, namely, launching, flight in space, re-entry, and final descent, must be considered when establishing need of attitude control for each type of vehicle such as ballistic missile, manned satellite, and hypersonic rocket boosted glider; factors to consider in obtaining attitude control and problems of re-entry.
Attitude control for space vehicles
Astronautics
Astronautics ; 4 , n 3
1959
2 pages
Article (Journal)
English
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Optimal attitude control of space vehicles
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