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This study focuses on designing a relative rendezvous trajectory for angles-only navigation between two satellites. The main purpose of this paper is to design a rendezvous trajectory which provides better observability for the whole mission period. The second purpose is to improve fuel consumption efficiency. For the trade-off between the observability maneuver and fuel consumption, it is important...
Using Fisher Information Matrix(FIM), the optimal trajectory which is generated in order to localize the specific target is obtained as optimal problem. However, it is more effective to use more vehicles with various sensor in order to gather information about target. So, since we just check how multi vehicles with various sensors by cooperative maneuver affect the trajectory in this paper. Analytical...
The genetic algorithms (GAs) have been recently used in many design problems including an orbit design and trajectory optimization problems due to their global search capability and the robust characteristics. Furthermore, the GAs do not require convenient analytical representations of the problem any more. For this reason, the GAs can provide good solutions to the orbital dynamics design problem,...
Using Fisher Information Matrix (FIM), the optimal trajectory to localize a specifc target is obtained as optimization problem. However, it is more effective to employ more vehicles with various sensors in order to gather suffcient information about the target. So, it is investigated how multi vehicles with different types of sensors by cooperative maneuver affect the trajectory in this paper. Clearly...
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