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1)  guidance miss distance
导航误差距离<火>
2)  guidance miss distance
导航误差距离
3)  error distance
误差距离
1.
Based on the existing study of incoherent dual point-source counteracting anti-radar missile (ARM),the attacking process of ARM was researched through analyzing the homing and moving theory of ARM,and the error distance of ARM disturbed by dual point-source was probed into.
结合现有非相干两点源抗反辐射导弹模型的研究成果,通过分析反辐射导弹的导引和运动机理,进一步细化了反辐射导弹的攻击过程,在此基础上对两点源干扰下的反辐射导弹误差距离进行了探讨。
2.
And then the error distance of ARM disturbed by dual point-source was probed into.
基于导弹运行轨迹,分别建立了导弹沿中垂线入射和以一定角度入射的动态跟踪模型,在此基础上对两点源干扰下的反辐射导弹误差距离进行了探讨。
4)  distance error
距离误差
1.
New manipulator calibration method based on screw theory and distance error;
基于旋量理论及距离误差的机械臂标定新方法
2.
In order to improve the precision while the new system corrects distance error,a new method was proposed by error analysis and emulation computation.
为了有效提高新系统在校正距离误差时的精度,通过误差分析、仿真计算,提出了舰炮校正距离误差的新方法。
3.
Constraint equations were constructed by using distance error model,and the actual geometric parameters of the robot were solved,and then these parameters were used in the modified kinematics model.
利用距离误差模型构造出机器人本体的约束方程,并求解出机器人的实际几何参数,进而将该参数应用于修正系统的运动学模型。
5)  navigation error
导航误差
1.
First,ground static deviation information of GPS/GLONASS orientation system is get and is regarded as modification error of shut down point parameters while real-timely navigating,then the impact deviation is gained by calculating trajectory,that is navigation error caused by ground static deviation is get.
首先获取了GPS/GLONASS定位信息接收系统的地面静态偏差信息,将地面静态偏差作为实时导航的关机点参数修正误差,接着解算弹道求落点偏差,得到了地面静态偏差引起导航误差的大小。
2.
The simulation result shows that: if single-axle rotating modulation is used,the error caused by bias of gyros/accelerators can be compensated effectively,while navigation error caused by the initial position/velocity/attitude error can not be compensated.
捷联惯性导航系统的旋转调制技术是一种自校正方法,它能在不使用外部信息的条件下,自动补偿陀螺漂移和加速度计零偏引起的系统导航误差。
3.
It is also proposed that the closed track is propitious to eliminate the majority of navigation error.
仿真结果说明这种方法能够有效提高导航系统精度,从仿真曲线还得到了闭合航路能够大幅度消除导航误差的结论。
6)  GNE Gross Navigational Error
总导航误差
补充资料:奥米加导航系统(见飞机双曲线导航系统)


奥米加导航系统(见飞机双曲线导航系统)
Omega navigation system

  Aomiiia daohang Xitong奥米加导航系统(omeg。。avigationsystem)见飞机双曲线导航系统。
  
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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