| タイトル | Hybrid near-optimal aeroassisted orbit transfer plane change trajectories |
| 本文（外部サイト） | http://hdl.handle.net/2060/19960028157 |
| 著者（英） | Calise, Anthony J.; Duckeman, Gregory A. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1994-01-01 |
| 言語 | eng |
| 内容記述 | In this paper, a hybrid methodology is used to determine optimal open loop controls for the atmospheric portion of the aeroassisted plane change problem. The method is hybrid in the sense that it combines the features of numerical collocation with the analytically tractable portions of the problem which result when the two-point boundary value problem is cast in the form of a regular perturbation problem. Various levels of approximation are introduced by eliminating particular collocation parameters and their effect upon problem complexity and required number of nodes is discussed. The results include plane changes of 10, 20, and 30 degrees for a given vehicle. |
| NASA分類 | Astrodynamics |
| レポートNO | 96N29216
NASA-TM-111446
NAS 1.15:111446 |
| 権利 | No Copyright |
