| タイトル | The analysis of a generic air-to-air missile simulation model |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940031931 |
| 著者（英） | Kaplan, Joseph A.; Chappell, Alan R.; Mcmanus, John W. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1994-06-01 |
| 言語 | eng |
| 内容記述 | A generic missile model was developed to evaluate the benefits of using a dynamic missile fly-out simulation system versus a static missile launch envelope system for air-to-air combat simulation. This paper examines the performance of a launch envelope model and a missile fly-out model. The launch envelope model bases its probability of killing the target aircraft on the target aircraft's position at the launch time of the weapon. The benefits gained from a launch envelope model are the simplicity of implementation and the minimal computational overhead required. A missile fly-out model takes into account the physical characteristics of the missile as it simulates the guidance, propulsion, and movement of the missile. The missile's probability of kill is based on the missile miss distance (or the minimum distance between the missile and the target aircraft). The problems associated with this method of modeling are a larger computational overhead, the additional complexity required to determine the missile miss distance, and the additional complexity of determining the reason(s) the missile missed the target. This paper evaluates the two methods and compares the results of running each method on a comprehensive set of test conditions. |
| NASA分類 | COMPUTER PROGRAMMING AND SOFTWARE |
| レポートNO | 94N36438
NASA-TM-109057
NAS 1.15:109057 |
| 権利 | No Copyright |
