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The first phase solves a series of single-target rendezvous problems for all departure-arrival object pairs to generate the elementary solutions, which provides candidate rendezvous trajectories.
To rapidly design three dimensional low-thrust safe trajectories for spacecraft orbit transfer and rendezvous problems, an analytic shape-based approach is proposed.
Most of the existing studies address rendezvous problems as a design of a search strategy to meet on the same channel at the same time.
To rapidly design low-thrust trajectories between coplanar orbits for the orbit transfer and rendezvous problems, an analytic shape-based approach is proposed.
This paper addresses the leaderless and leader follower rendezvous problems of multiple autonomous surface vehicles subject to dynamical uncertainties and ocean disturbances.
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This paper takes a revisit of the fuel-optimal four-impulse rendezvous problem near circular orbits.
This paper studies the distributed rendezvous problem of multi-agent systems with novel event-triggered controllers.
Based on Lyapunov theory, the autonomous rendezvous problem is regarded as an asymptotic stabilization problem.
A low-earth orbit multiple-impulse rendezvous problem is used as an example.
This paper proposes a two-phase framework to obtain a near-optimal solution of multi-target Lambert rendezvous problem.
A simple way to solve the rendezvous problem is by using a common control channel (CCC) [4].
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