Abstract
The design and planning of space trajectories is a challenging problem in mission analysis. In the last years global optimisation techniques have proven to be a valuable tool for automating the design process that otherwise would mostly rely on engineers’ expertise. The paper presents the optimisation approach and problem formulation proposed by the team Strathclyde++ to address the problem of the 9th edition of the Global Trajectory Optimisation Competition. While the solution approach is introduced for the design of a set of multiple debris removal missions, the solution idea can be generalised to a wider set of trajectory design problems that have a similar structure.
Original language | English |
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Pages (from-to) | 57-70 |
Number of pages | 14 |
Journal | Acta Futura |
Issue number | 11 |
DOIs | |
Publication status | Published - 9 Jan 2018 |
Keywords
- global trajectory optimisation competition
- GTOC
- European Space Agency
- low Earth orbit (LEO)
- Kessler run
- debris removal
- space missions
- astronautics