This paper addresses a prototype of a maneuver decomposition algorithm developed by the Genesis Navigation Team at JPL. The algorithm described herein is an early prototype designed to support navigation analyses and to provide the basis for later development of operational software by the Spacecraft Team. The basis algorithm is applicable to any spin-stabilized spacecraft with axisymmetric thrusters.
Prototype maneuver decomposition algorith for genesis
2001-09-06
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Englisch
Prototype Maneuver Decomposition Algorithm for Genesis (AAS 02-001)
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