姿态参数的英文

• attitude parameter

• "姿态"英文翻译    gesture; posture; one's bear ...
• "参数"英文翻译    parameter
• "姿态参照系" 英文翻译 :    attitude reference system
• "动态参数" 英文翻译 :    dynamic parameter
• "静态参数" 英文翻译 :    static parameter
• "静态参数值" 英文翻译 :    static value
• "模态参数" 英文翻译 :    modal parameter; mode shape parameter
• "生态参数" 英文翻译 :    ecological optimum
• "状态参数" 英文翻译 :    condition parameter; conditionparameter; property of state; state parameter; state variable; status parameter
• "状态参数值" 英文翻译 :    quantity of state
• "组态参数" 英文翻译 :    configuration parameters
• "动态参数编码" 英文翻译 :    dynamic parameter encoding dpe
• "动态参数测试" 英文翻译 :    dynamic parametric test
• "湖泊形态参数" 英文翻译 :    morphometric parameter of lake
• "久航状态参数" 英文翻译 :    maximum endurance settings
• "油层动态参数" 英文翻译 :    reservoir operating parameter
• "基本姿态参考系统" 英文翻译 :    primary attitude reference system
• "动态参数，动态型参数" 英文翻译 :    dynamic parameter
• "晶体管动态参数" 英文翻译 :    transistor dynamic parameter
• "静态参数测试仪" 英文翻译 :    static parameter tester
• "陀螺罗盘姿态参考系统" 英文翻译 :    gyrocompass attitude reference system (gars)
• "动态参数测试与分析技术" 英文翻译 :    dynamic parameters measurement and analysis technique
• "发动机空中慢车状态参数" 英文翻译 :    flight idling power conditions
• "发协机慢车状态参数" 英文翻译 :    idling power conditions
• "光纤模态参数测试器" 英文翻译 :    optical fiber mode field parameters test equipment

• And with the rapid development of dsp technology , it would become true that acquire the real - time attitude parameters
  加上dsp技术的高速发展，实时的、正确的获得高精度的姿态参数已经成为可能。
• For the field of the measurement and control system , the attitude measurement of plat is the very important embranchment all along . but the conventional attitude measurement equipment is too expensive to be put into practice
  实时的获得载体平台的姿态参数一直是测控领域一个很重要的研究方向，但是传统测控方法在处理速度和成本等方面存在诸多弊端。
• It is very useful to compute the real - time attitude parameters . finally , the paper gave the result of simulation and hardware design . by comparing and analyzing the result , the feasibility of the design is contenting
  这对于实时的获得载体的姿态参数是很重要的论文的第五部分给出了软件仿真的结果和硬件系统的设计思路，并对仿真的结果进行了分析和比较，以证明该技术的可行性。
• 3 ) we research the attitude character of the radar target in the midcourse , analyse the rotation of the target in the midcourse on the basis of the attitude dynamics of space target . with the data of the trajectory in the midcourse , we calculate attitude parameter of the ballistic missile
  在空间目标姿态动力学的基础上分析中段目标的进动,结合中段轨道数据,给出了中段弹道导弹的姿态参数(目标雷达视线角)的计算结果。
• In this dissertation , we make a deep research on the trajectory character and attitude character of the radar target in the midcourse . much work has been done to simulate the trajectory and attitude , we get the attitude parameter of radar target by coordinate transferring
  本文深入研究了雷达目标中段的轨道特性和姿态特征,在弹道导弹的弹道和姿态仿真方面做了大量的工作,通过坐标转换的方式完成了对目标姿态参数的计算。
• Based on the study status at present , the dissertation determines the flight simulation system combined with distributed virtual reality ( dvr ) and traditional simulation methods as the emphasis . according to the basis design principles of dvr , a design scheme of the whole simulation system is proposed . through studying several coordinate systems of the flight dimension and the conversion among them , the article carries out a conversion of the parameters from the flight dimension to the virtual scene
  在分析分布式虚拟现实系统基本设计思想的基础上，确立了系统的总体设计方案；深入研究了飞行空间的几种坐标体系及其相互之间的转换，提出了一种将飞行姿态参数转化到虚拟三维空间的变换方法；利用vrml建立了较为完善的三维虚拟飞行场景；分析了vrml动画的产生和与用户交互机制，实现对场景动画的控制；建立了虚拟飞行场景与外部java程序的数据接口，并进一步实现了对远程数据库中飞行数据的访问。