| タイトル | A trajectory planning scheme for spacecraft in the space station environment |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910007758 |
| 著者（英） | Soller, Jeffrey Alan; Ellis, Stephen R.; Grunwald, Arthur J. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | Simulated annealing is used to solve a minimum fuel trajectory problem in the space station environment. The environment is special because the space station will define a multivehicle environment in space. The optimization surface is a complex nonlinear function of the initial conditions of the chase and target crafts. Small permutations in the input conditions can result in abrupt changes to the optimization surface. Since no prior knowledge about the number or location of local minima on the surface is available, the optimization must be capable of functioning on a multimodal surface. It was reported in the literature that the simulated annealing algorithm is more effective on such surfaces than descent techniques using random starting points. The simulated annealing optimization was found to be capable of identifying a minimum fuel, two-burn trajectory subject to four constraints which are integrated into the optimization using a barrier method. The computations required to solve the optimization are fast enough that missions could be planned on board the space station. Potential applications for on board planning of missions are numerous. Future research topics may include optimal planning of multi-waypoint maneuvers using a knowledge base to guide the optimization, and a study aimed at developing robust annealing schedules for potential on board missions. |
| NASA分類 | ASTRONAUTICS (GENERAL) |
| レポートNO | 91N17071
A-90287
NAS 1.15:102866
NASA-TM-102866 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/134245 |
