Abstract A method for simulating a flexible spacecraft motion using Lagrange’s quasivelocity formulation is considered. An algorithm of quasivelocity formation by Walsh’s means is proposed. This method can be used to evaluate a quasistatic microacceleration field component in the spacecraft internal environment.
Simulation of a flexible spacecraft motion to evaluate microaccelerations
Russian Aeronautics (Iz VUZ) ; 52 , 4 ; 484-487
01.12.2009
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Simulation of a flexible spacecraft motion to evaluate microaccelerations
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