动态滑翔动力学建模与风梯度能量获取
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国家863计划资助项目(2014AA7054035)


Dynamics modeling of dynamic soaring and energy gaining from the wind gradient
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    摘要:

    为简化问题描述和便于数学操作,对无动力飞机的动态滑翔问题做了假设,并在这些假设下建立了无动力飞机动态滑翔的动力学模型,即三维速度空间中只有一个输入变量的常微分方程组。之后,从理论上得到了这个三维速度空间中机械能可以增加的最大范围,即能增纺锤体内部,并推导出最大的机械能增加率。得出更大的风梯度、更小的阻力系数和更小的面质比更加有利于飞机获取能量的结论,该结论加深了对动态滑翔能量观点的认识,对实践有指导意义。

    Abstract:

    In order to simplify the description of the problems and to be convenient for mathematical manipulation, a series of hypotheses about the dynamic glide problem of unpowered aircraft were made. Under these hypotheses, a dynamics model of dynamic soaring, which is a 3-dimentional ordinary differential equations in the velocity space with a single input, was built. The largest growing area of mechanical energy in this velocity space, which is called energy-gained spindle, was obtained theoretically and the maximum rate of energy increasing was also deduced. The conclusion that the larger wind gradient, the smaller drag and the smaller area-mass ratio are more in favor of gaining energy for the engines aircraft gives a deeper understanding of the dynamic soaring energy and it can help the practice. 

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单上求,侯中喜,朱炳杰,等.动态滑翔动力学建模与风梯度能量获取[J].国防科技大学学报,2015,37(4):45-49.
SHAN Shangqiu, HOU Zhongxi, ZHU Bingjie, et al. Dynamics modeling of dynamic soaring and energy gaining from the wind gradient[J]. Journal of National University of Defense Technology,2015,37(4):45-49.

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  • 收稿日期:2014-04-10
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  • 在线发布日期: 2015-09-01
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