| 带推力矢量作战飞机常规机动性能评估 |
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| 引用本文： | 华玉光,徐浩军,刘凌,葛志浩.带推力矢量作战飞机常规机动性能评估[J].飞行力学,2006,24(4):6-8,13. |
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| 作者姓名： | 华玉光 徐浩军 刘凌 葛志浩 |
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| 作者单位： | 空军工程大学,工程学院,陕西,西安,710038 |
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| 基金项目： | 教育部优秀青年教师资助计划 |
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| 摘 要： | 建立了带推力矢量作战飞机的运动方程,确定了垂直面和水平面内常规机动性能的评估指标。以半筋斗和加力盘旋为例计算了带推力矢量作战飞机的常规机动性能,并对带推力矢量作战飞机常规机动性能的变化进行了评估。结果表明,作战飞机带推力矢量后,完成半筋斗和加力盘旋机动动作的空间减小,时间缩短,机动性能得到了提高。
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| 关 键 词： | 作战飞机 推力矢量 常规机动性能 |
| 文章编号： | 1002-0853（2006）04-0006-03 |
| 收稿时间： | 2005-10-27 |
| 修稿时间： | 2005-10-272006-08-21 |
Routine Maneuver Performance Evaluation of a Fighter with Thrust Vector |
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| HUA Yu-guang,XU Hao-jun,LIU Ling,GE Zhi-hao.Routine Maneuver Performance Evaluation of a Fighter with Thrust Vector[J].Flight Dynamics,2006,24(4):6-8,13. |
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| Authors: | HUA Yu-guang XU Hao-jun LIU Ling GE Zhi-hao |
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| Abstract: | The Dynamic equations of a fighter with thrust vector are built,the evaluation standards of routine maneuver performance in horizontal and vertical are ascertained.In two examples of half-flip and augmented circling,routine maneuver performance is calculated and the changes for thrust vector are evaluated.The results show that the fighter with thrust vector have smaller radius,shorter time and better maneuver performance. |
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| Keywords: | fighter thrust vector routine maneuver performance |
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