Abstract
This work examines a strategy for combining two heuristic methods, Differential Evolution (DE) and Particle Swarm Optimization (PSO) to better address the problem of stagnation when solving time-optimal slew-maneuver problems with path constraints. Several approaches are considered, including the use of only PSO or DE, and use of PSO with DE applied to some iterations. Applying a newer form of DE, in which random fractions of the vector-difference components are employed, stagnation is not evident, but the computational time is greater. The combined PSO/DE method handles the stagnation very well, with a 40% reduction in computation time compared with just DE.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 246-259 |
| Number of pages | 14 |
| Journal | Acta Astronautica |
| Volume | 148 |
| DOIs | |
| State | Published - Jul 2018 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
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