| タイトル | A man in the loop trajectory optimization program (MILTOP) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750005826 |
| 著者（英） | Reinfields, J. |
| 著者所属（英） | Interactive Computer Systems, Inc. |
| 発行日 | 1974-01-01 |
| 言語 | eng |
| 内容記述 | An interactive trajectory optimization program is developed for use in initial fixing of launch configurations. The program is called MILTOP for Man-In-the-Loop-Trajectory Optimization-Program. The program is designed to facilitate quick look studies using man-machine decision combinations to reduce the time required to solve a given problem. MILTOP integrates the equations of motion of a point-mass in 3-Dimensions with drag as the only aerodynamic force present. Any point in time at which an integration step terminates, may be used as a decision-break-point, with complete user control over all variables and routines at this point. Automatic phases are provided for different modes of control: vertical rise, pitch-over, gravity turn, chi-freeze and control turn. Stage parameters are initialized from a separate routine so the user may fly as many stages as his problem demands. The MILTOP system uses both interactively on storage scope consoles, or in batch mode with numerical output on the live printer. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 75N13898
NASA-CR-120560 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/191787 |
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