In this paper aerodynamic characteristics of maneuvering reentry vehicle of cruciform configuration and bifurcate configuration are compared by means of the wind tunnel test results.
利用典型状态的风洞试验结果对十字布局与叉字布局再入机动飞行器的气动特性进行了分析与比较。
Programming maneuvering flight guidance scheme about reentry vehicle is presented in this paper.
文提出一种关于再入飞行器程序机动飞行的制导方案。
An optimal guidance law for reentry vehicle with high altitude maneuvering on downward phase is studied.
研究了在降弧段进行高空机动的再入飞行器最优制导律。
The guidance method satisfies terminal angular constraint as reentry vehicle hitting target, but also ensures minimum loss of maneuvering velocity for reentry vehicle.
该方法利用最优控制理论的思想方法，不仅使飞行器命中目标时满足了终端角度约束的条件，而且保证了再入飞行器机动速度损失最小。
Variable bend tail concept may be one of the possible approaches for satisfying the maneuvering requirement of hypersonic reentry vehicle.
可变弯尾飞行器的气动方案是高超声速机动的潜在可行方案。
Variable bend tail concept may be one of the possible approaches for satisfying the maneuvering requirement of hypersonic reentry vehicle.
可变弯尾飞行器的气动方案是高超声速机动的潜在可行方案。
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