| 某型无人机发射段飞行轨迹研究 |
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| 引用本文： | 周同礼.某型无人机发射段飞行轨迹研究[J].南京航空航天大学学报,1988(3). |
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| 作者姓名： | 周同礼 |
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| 摘 要： | 用火箭助推起飞是广泛应用的无人机起飞的一种方式,它和用起飞车助跑起飞方式相比有一些优越之处。本文总结了在某型无人机采用火箭助推起飞时的飞行轨道研究中探讨过的几个问题,包括发射参数的选择原则和发射起飞过程中的一些特殊问题.如力矩平衡问题,无人机和滑轨之间相对运动问题等。
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| 关 键 词： | 无人驾驶飞机 轨道 起飞助推器 发射段 |
A Study of the Flight Trajectory of Pilotless Aircraft in the Launch Posture |
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| Zhou Tongli.A Study of the Flight Trajectory of Pilotless Aircraft in the Launch Posture[J].Journal of Nanjing University of Aeronautics & Astronautics,1988(3). |
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| Authors: | Zhou Tongli |
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| Institution: | Zhou Tongli |
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| Abstract: | A boosted rocket is widely used during the take-off of a pilotless aircraft. It has some advantages over the launch vehicle used for take-off. In this paper some problems encountered in the study of flight trajectory of a pilotless aircraft are summarized as a boosted rocket is used for takeoff. The selection principle of the launch parameters and particular problems in launching, such as, the balancing of moments and the relative motions between the pilotless aircraft and the slide are also included in these problems. |
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| Keywords: | pilotless aircraft trajectory launching booster launching posture |
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