| 有翼飞行器最大横向航程的最优三维再入机动轨道 |
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| 引用本文： | 宋淑萍.有翼飞行器最大横向航程的最优三维再入机动轨道[J].佳木斯大学学报,1997(1). |
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| 作者姓名： | 宋淑萍 |
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| 作者单位： | 佳木斯工学院基础部 |
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| 基金项目： | 国家863计划重点课题 |
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| 摘 要： | 在平衡滑翔假设条件下，使用一组无量纲的运动方程，取满足最大过载和热流峰值约束条件的最大升阻比E=2，计算了有翼飞行器最大横向航程的最优再入机动轨道．
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| 关 键 词： | 有翼飞行器 轨道 航程 |
OPTIMAL THREE-DIMENSION REENTRY MANOEUVER TRAJECTORY WITH MAXIMUM CROSS RANGE FOR SHUTTLE VEHICLE |
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| Song Shuping.OPTIMAL THREE-DIMENSION REENTRY MANOEUVER TRAJECTORY WITH MAXIMUM CROSS RANGE FOR SHUTTLE VEHICLE[J].Journal of Jiamusi University(Natural Science Edition),1997(1). |
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| Authors: | Song Shuping |
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| Institution: | Jiamusi Institute of Technology 154007 |
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| Abstract: | The maximum lift- to- drag ratio is calculated to be E'=2,through a set of dimensionless equations, under the conditions of equilibrium glide andmaximum load factor and peak heating rate in this paper. And the optimal three-dimension reentry manoeuver trajectory with maxmum cross range for shuttle vehicle iscalculated as well. |
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| Keywords: | shuttle vehicle trajectory flying range |
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