根据中段弹道目标的运动学特性，结合室内缩比模型RCS静态测量数据，提出了一种雷达目标动态rcs仿真的方法。
According to the kinetic characteristic of targets in midcourse and the RCS data of static measurement of the model, a simulation method for dynamic RCS data of radar targets is proposed.
根据以上设计，结合导引头模型、复合控制系统模型、弹体运动学模型、目标机动模型，给出上述设计的仿真结果。
Finally, present the simulation result of above design combining seeker handing-off model, compound control system model, projectile body kinematics model and target maneuver model.
提出一种基于运动学参数的自适应IMM算法，进行高速高机动目标跟踪。
This paper proposes one kind of adaptive IMM algorithm based on kinematics parameters used for tracking the high speed and high maneuvering target.
目标在空中的姿态及轨迹由动力学和运动学方程确定。
The pose and trajectory of the flying radar target are calculated by means of dynamical and kinematical equations.
首先在相对运动学的基础上建立了归一化的导弹—目标的运动学模型，然后利用变结构控制理论设计了导引律。
The unitary missile target kinematics model is established based on the relative kinematics firstly. Then the guidance law is designed using variable structure system theory.
结构参数优化是并联机器人运动学设计的最终目标。
Parameter optimization is a final aim of the design of parallel robot.
基于三维弹目相对运动学的非线性关系，将目标机动作为系统扰动，建立了弹目相对运动的数学模型。
The mathematic model is built according to the three-dimensional relationship between the missile and the target whose acceleration is introduced as disturbance.
利用试验仿真方法采取多目标多因素优化方式，得出了最优的前悬架结构参数，优化了前悬架的运动学特性。
Test simulation was used to derive the optimal structural parameters and optimize the kinematics of the suspension by a multi-objective and multi-variable optimization.
利用试验仿真方法采取多目标多因素优化方式，得出了最优的前悬架结构参数，优化了前悬架的运动学特性。
Test simulation was used to derive the optimal structural parameters and optimize the kinematics of the suspension by a multi-objective and multi-variable optimization.
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