Optimizing multi-rendezvous spacecraft trajectories: $\Delta V$ matrices and sequence selection
Aleksandar Petrov, and Ron Noomen

TL;DR
This paper introduces a novel approach to optimize multi-rendezvous spacecraft trajectories by using $\Delta V$ matrices and sequence selection, enabling automated and efficient mission planning without extensive pruning.
Contribution
The research develops a method leveraging $\Delta V$ matrices for automated sequence optimization in multi-rendezvous missions, replacing traditional heuristic pruning techniques.
Findings
$\Delta V$ matrices effectively represent transfer costs between celestial bodies.
Sequence optimization can be formulated as a shortest path problem on a graph.
The approach incorporates waiting times and transfer variability into the matrices.
Abstract
Multi-rendezvous spacecraft trajectory optimization problems are notoriously difficult to solve. For this reason, the design space is usually pruned by using heuristics and past experience. As an alternative, the current research explores some properties of matrices which provide the minimum values for a transfer between two celestial bodies for various times of departure and transfer duration values. These can assist in solving multi-rendezvous problems in an automated way. The paper focuses on the problem of, given a set of candidate objects, how to find the sequence of objects to rendezvous with that minimizes the total required. Transfers are considered as single algebraic objects corresponding to matrices, which allow intuitive concatenation via a generalized summation. Waiting times, both due to mission requirements and prospects for…
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Taxonomy
TopicsSpace Satellite Systems and Control · Optimization and Search Problems · Spacecraft Dynamics and Control
