摘要
In the ground simulation of air to air combat state, maneuvering flight generator is required to control the maneuvering fighter. Based on the theory of fighter's maneuvering flight, the principle of designing maneuvering flight generator was analyzed. The linearized mathematical method was used to describe the relationships between the maneuvering flight commands and the flying parameters of fighter. Then, the mathematical model of flight path generator was estimated. Flight path simulation indicated the rationality of the mathematical model. The principle of designing maneuvering flight generator could also be used in other states of fighter's combat simulation.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 448-451 |
| 页数 | 4 |
| 期刊 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| 卷 | 23 |
| 期 | 4 |
| 出版状态 | 已出版 - 8月 2005 |
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