N-body problem and special perturbation techniques; consideration of n-body problem, its application to problem of determining motion of spacecraft, and technique available for its solution; techniques for handling equations and for integrating equations numerically are discussed.
Guidance, flight mechanics and trajectory optimization -- 6
NASA CR
NASA Contractor Reports ; n 1005
1968
113 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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Engineering Index Backfile | 1968
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