Problem of rendezvous is studied from point of view of injection into sufficiently precise trajectory; in event of primary guidance mode failure, simple secondary guidance technique is needed to satisfy rendezvous objective; guidance law is developed which uses predetermined compensation; 4 measurements are made during powered flight of vehicle, and simple calculations and corrective actions are used to adjust vehicle motion.
"t1 compensation" guidance law for launch of space vehicles
Am Astronautical Soc -- Advances Astronautical Sciences
1963
28 pages
Article (Journal)
English
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