| 无人机爬升航迹优化设计研究 |
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| 引用本文： | 沈延航,周洲.无人机爬升航迹优化设计研究[J].飞行力学,2004,22(3):28-30. |
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| 作者姓名： | 沈延航 周洲 |
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| 作者单位： | 西北工业大学,365研究所,陕西,西安,710072 |
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| 摘 要： | 为改进无人机的飞行性能，应用可变误差多面体法求解了在垂直平面内的最经济和最快爬升轨迹。计算结果表明，经优化后的爬升航迹可以节省燃油，延长无人机的续航时间和有效任务时间，具有较好的性能收益。
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| 关 键 词： | 无人机 可变误差多面体法 航迹优化 仿真 |
| 文章编号： | 1002-0853(2004)03-0028-03 |
| 修稿时间： | 2003年7月31日 |
Research on Method in Calculation of Optimal Climb Trajectory of an UAV |
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| SHEN Yan-hang,ZHOU Zhou.Research on Method in Calculation of Optimal Climb Trajectory of an UAV[J].Flight Dynamics,2004,22(3):28-30. |
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| Authors: | SHEN Yan-hang ZHOU Zhou |
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| Abstract: | For improving the performance in flight of an attack UAV,this paper strives for the optimal climb trajectory of the attack UAV in the vertical plane, using the flexible tolerance polyhedron method. The calculating results state that the fuel of the attack UAV can be saved and the endurance of it can be lengthened or the final altitude predetermined can be climbed fast, and there is the better profit in performance according to the climbing trajectory optimized. |
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| Keywords: | UAV flexible tolerance polyhedron method trajectory optimization simulation |
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