最后，进行了六自由度仿真，结果表明：设计的制导律及控制方案是合理、有效的，易于实现。
Finally, 6 DOF simulations are made based on a kind of reentry aerocraft. The results show that the proposed control scheme and the guidance law are rational, efficient and easy for implementation.
研究了空天飞行器超声速和高超声速飞行条件下六自由度仿真模型，该模型包含了完整的六自由度动力学方程和运动方程。
Six Degrees of Freedom model and simulation of an aerospace vehicle is presented, which includes the whole of kinetic equations and motion equations.
最后给出了单独使用振荡天平数据、综合使用振荡天平试验数据和旋转天平数据的六自由度仿真结果，以及相应的试飞结果。
This paper integrated factor in synthetical using of data, and finally gives six - degree - of - freedom simulation results by independently using data of oscillating balance, synthetical…
提出了弹射座椅全姿态关系式，介绍了在不同弹射条件下座椅全姿态关系式的取值范围以及六自由度仿真中座椅姿态参数初始值的传统选取方法。
In order to determine the initial value of seat attitude parameter in 6 DOF function, an ejection seat all-attitude formula was presented in this paper.
将设计好的制导控制算法嵌入六自由度弹道模型中进行验证，仿真结果表明了此快速仿真架构的正确性和制导、控制方案的可行性。
The GNC algorithms designed are embedded in the trajectory model. The results show that the simulation structure is valid and the GNC schemes are feasible.
本文简要介绍了再入体六自由度控制系统半实物仿真的系统结构与软件系统设计，并探讨了相应的仿真技术途径。
In this paper, system structure and software design of reentry vehicle Sir -dof semi physical simulation are introduced briefly, and corresponding simulation technical methods is discussed.
根据时标分离的原则，设计飞行器的快回路和慢回路控制器，并进行全包线六自由度非线性仿真。
And based on the time-scale separation principle, divided the control system into fast loop and slow loop, finish the six degrees of freedom nonlinear coordination simulation.
最后用六自由度弹道数字仿真结果同近似计算结果作了比较，比较结果表明了近似分析的可行性。
Finally, we compare six degrees of freedom simulation results of ballistic re-entry missiles motion with the computing results of approximate formula. The comparison shows the feasibility...
为了实现六自由度摇摆台结构的优化设计、实时仿真和控制，对六自由度摇摆台运动学和动力学特性作全面的了解是很有必要的。
For accomplishing its optimizing design, real simulation and control, you must have a full knowledge of the manipulating structure's kinematics and dynamics.
基于虚拟样机技术对六自由度关节臂式坐标测量机的测量空间进行研究和仿真，建立了六自由度关节臂式坐标测量机的测量运动学数学模型和虚拟样机模型。
Based on virtual prototyping technology, the six-degrees of freedom Articulated Coordinate Measuring Machine (A-CMM) is investigated, and the measure space of the A-CMM is analyzed and simulated.
基于系统键合图模型，利用20 -SIM仿真软件，对六自由度转台的一个支路进行了建模与仿真。
Based on the key matches diagram of system, made use of 20-sim imitation software to construction model and imitation for a byroad of six free degree rotation stand.
针对飞行器制导和姿态控制分立式三自由度仿真存在的不足 ，研究并给出了飞行器的六自由度运动模型 。
To counter the disadventage of three degree of freedom simulation of a flying vehicle, the six degree of freedom movement mathematical model is presented.
六自由度的仿真实验表明弹道设计满足任务要求，验证了弹道设计的正确性和合理性。
The results of the six - dimension simulation indicates that the design meets all the task requirements, which validates the correctness and rationality of trajectory design.
针对控制系统采用侧喷流发动机和栅格舵的新型小型多级固体运载火箭开展六自由度弹道仿真研究。
This article studies the six-degree-of-freedom trajectory simulation of small multiple stage solid launch vehicles with control systems using lateral jet thrusters and grid fins.
六自由度运动模拟器作为空间对接过程半物理仿真试验系统的关键设备之一，其位姿误差直接影响整个系统的仿真精度。
The 6-dof motion simulator is one of the most pivotal equipments in the spacecraft docking simulation, and the precision of the simulation system is determined by its pose error.
文中在对弹道追踪导引律原理进行简单介绍的基础上，在六自由度弹道模型上进行了蒙特卡洛仿真打靶试验。
Based on the brief introduction of the theory of trajectory tracking guidance law, Monte Carlo simulation fire tests were done with the 6 degree-of-freedom trajectory simulation model.
潜艇水下运动是六个自由度的多姿态运动，建立空间运动方程数学模型是计算机仿真时对其进行比较准确的描述和对运动状态进行仿真研究的关键。
The submarine underwater motion is the 6d motion multi-stance movement. It requires quite exact description and dynamic simulation research. The key technology is to create submarine motion equation.
仿真结果表明，与实际飞行试验数据达到非常好的拟合，说明采用六自由度的制导控制系统的数学模型进行设计的正确性。
Numerical simulation results for sample engagement scenarios are given. It shows that simulation results are very close to the actual flight test results. So …
仿真结果表明，与实际飞行试验数据达到非常好的拟合，说明采用六自由度的制导控制系统的数学模型进行设计的正确性。
Numerical simulation results for sample engagement scenarios are given. It shows that simulation results are very close to the actual flight test results. So …
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