It is shown how a method for maneuver design during the Jovian satellite tour phase of the Galileo mission requires a full-scale redesign of the tour at each maneuver. Software was developed to provide insight into the statistical properties of this process; it is based on the use of linear perturbations to provide trajectory propagation and a least squares representation of the optimization. The result is a Monte Carlo program, making it possible to evaluate the proposed strategy.
Linear statistical analysis of maneuver optimization techniques
AAS/AIAA Astrodynamics Conference ; 1987 ; Kalispell, MT, United States
1988-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
NTRS | 1973
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