Multi-objective minimum time optimal control for low-thrust trajectory design
We propose a reachability approach for infinite and finite horizon multi-objective optimization problems for low-thrust spacecraft trajectory design. The main advantage of the proposed method is that the Pareto front can be efficiently constructed from the zero level set of the solution to a Hamilto...
| Váldodahkkit: | , , |
|---|---|
| Materiálatiipa: | Conference item |
| Giella: | English |
| Almmustuhtton: |
IEEE
2022
|