Monte Carlo technique was used to study relative performance of three methods of scheduling corrective thrust impulses in presence of various assumed inaccuracies in measuring velocity and flight-path angle and in obtaining desired thrust impulse; comparison of methods and results.
Study of guidance of space vehicle returning to braking ellipse about earth
NASA -- Tech Note
1960
65 pages
Aufsatz (Zeitschrift)
Englisch
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Earth Entry Vehicle For Returning Samples From Mars
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