所设计的再入机动弹道能满足机动弹头对姿态、热流和速度的要求。
The designed maneuver reentry trajectory can meet the demands of attitude, heat flux and velocity for the warhead.
建立了再入机动弹道数学模型，给出了气动力系数为速度、迎角、高度的函数拟合式，进行了最佳再入机动弹道设计和仿真计算。
The mathematical model of reentry maneuvering trajectory is established. The fitting expression of aerodynamic coefficient function on velocity, attack of Angle and altitude is presented.
阐明了针对大空域机动反舰导弹飞行空域大、速度变换范围大的特点，采用增益调度的方法设计其控制系统。
For Large aerospace maneuvering anti-ship missiles(LAMASM), which fly in large aerospace with velocity varies in large range, a gain schedule autopilot is designed.
目的：分析机动医疗方舱舱室温度场和气流速度场的分布状态并设计合理的舱室温度环境。
Objective:To analyze the distribution of air thermal field and velocity field inside mobile medical shelters and to redesign a reasonable thermal environment in them.
由于本算法能够估计出目标的法向和切向加速度，进行适当的模型集设计后，可以实现对复杂、快速机动目标的全过程跟踪，具有可扩展性的应用前景。
Because this algorithm can estimate the normal and tangent acceleration, it may be used to implement the tracking for the complexly and highly maneuvering target after appropriate model-set design.
我们很容易使你的相机设计简化，降低设备的足迹，并帮助机动速度次市场。
We make it easy to simplify your camera designs, reduce the device footprint, and help maneuver faster times to market.
这种模型可以采用和直流电动机动态设计同样的原理进行电流环及速度环的设计。
This model permits the design of the current and speed control loops to adopt the same principles as the dynamic design of armature DC motor drives.
实验证明，样机动作连贯，速度均匀，设计合理，可适用于多种自动控制领域。
The experiments prove that this motor can be widely used in various auto - control fields because of its consistent operation, uniform speed and reasonable design.
为了增加速度和机动性，雅克3的机身被设计得尽可能轻巧。
The Yak-3 airframe was created as light as possible to save weight and gain more speed and manoeuvrability.
实验结果表明，所设计的控制方案具有机动速度快、超调小，在机动过程中能抑制挠性板振动等优点。
The experimental results show that the control strategy has small overshoot and fast slew maneuver with simultaneous vibration suppression.
实验结果表明，所设计的控制方案具有机动速度快、超调小，在机动过程中能抑制挠性板振动等优点。
The experimental results show that the control strategy has small overshoot and fast slew maneuver with simultaneous vibration suppression.
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