Simulated annealing is used to solve a minimum fuel trajectory problem in the space station environment. The environment is unique because the space station will define the first true multivehicle environment in space. The optimization yields surfaces which are potentially complex, with multiple local minima. Because of the likelihood of these local minima, descent techniques are unable to offer robust solutions. Other deterministic optimization techniques were explored without success. The simulated annealing optimization is capable of identifying a minimum-fuel, two-burn trajectory subject to four constraints. Furthermore, the computational efforts involved in the optimization are such that missions could be planned on board the space station. Potential applications could include the on-site planning of rendezvous with a target craft of the emergency rescue of an astronaut. Future research will include multiwaypoint maneuvers, using a knowledge base to guide the optimization.
Simulated annealing in orbital flight planning
1990-12-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Introduction to orbital flight planning (1)
NTRS | 1981
|Introduction to Orbital Flight Planning (1)
NTIS | 1981
|Aircraft configuration and flight profile optimization using simulated annealing
Online Contents | 1999
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