The application of genetic algorithm is discussed in the problem of minimum-fuel consumption orbit manoeuvre of spacecraft. First, the method of operation is introduced. Two examples are then given: one is soft-landing of a lunar probe from lunar satellite orbit to lunar surface; and the other is orbit manoeuvre of lunar probe from a selenocentric hyperbolic orbit to a selenocentric circular orbit. It is shown that the genetic algorithm has good convergence property and high accuracy.
Use of genetic algorithm in optimal orbit manoeuvre
01.01.2000
356839 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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