所以有必要研究动基座的运动对光电设备的附加影响。
Therefore, it is necessary to study appendant effect of moving bases movement on the electro-optical equipments.
提出了一种新的基于合作目标的动基座传感器误差绝对配准方法。
A novel bias estimation method for solving maneuvering sensor bias correction problems based on cooperation target is proposed.
潜望式仪器在动基座上实现瞄准线稳定时，会存在较明显的像倾斜。
The image tilt is occurred at stabilizing the line of sight of periscope instrument on moving platform.
论文研究的主要内容是舰载机的动基座传递对准技术及其相关问题。
The main contents of the thesis are the technology of in-motion alignment and its related problem.
本文针对精确快速动基座对准的要求，作了以下几个方面的研究： 1。
The accuracy and rapidity of initial alignment are greatly concerned with the property of the inertial system.
摇摆状态下的捷联惯导初始对准，由于动基座情况下干扰较大，造成对准精度下降。
The accuracy of initial alignment for SINS is decreased as the large disturbance on swaying base.
针对捷联惯导系统的动基座初始对准问题，提出了一种新的动基座快速传递对准方案。
A new approach to transfer alignment for the initial alignment of Strapdown inertial navigation systems on moving base was put forward.
仿真结果表明，该方法实现简单，收敛速度快，可以实现单部动基座传感器的偏差估计。
The simulation results show the approach can be easily carried out and has the rapid convergence rate, which can estimate the biases of single maneuvering sensor.
同时，针对初始对准对准精度与快速性的要求，建立了动基座传递对准精确的非线性滤波模型。
Meanwhile, an accurate nonlinear filter model for moving base alignment is built, which meets the requirements of alignment velocity and accuracy in air-to-air missiles.
推导了动基座潜望式仪器瞄准线稳定时产生的像倾斜公式，分析了像倾斜的特性，得出了几点有意义的结论。
The formulas of image tilt are derived. The characteristics of the image tilt are analyzed. Some reasonable conclusions are drew.
该对准方法解决了动基座上方位快速对准的难题，大大降低了对载体的机动要求，同时为陀螺测漂提供了手段。
This method solves the problem of rapid azimuth alignment on the moving base, dramatically reduces the requirement of carrier's movement and gives a means of measure gyroscope drift.
舰载机惯导系统对对准精度、对准时间的要求及其所处的复杂环境使得舰载机的动基座对准问题变得比较困难。
The aim at alignment accuracy and time and the complicated environment made the carrier aircraft in-motion alignment difficulty.
利用最优平滑技术对惯导系统动基座对准效果进行评估，是分析导弹系统的制导精度和惯导系统自身器件性能的有效方法。
Using optimal smoothing technology to test and evaluate the accuracy of in-flight alignment is an available method to analysis the performance of INS.
通过建立动基座对准速度匹配的系统模型，对影响传递对准的一些重要因素如杆臂效应、挠曲振动等进行了分析，按照既定的载机机动方案采集飞行数据进行离线仿真。
By establishing the system model of moving-base alignment velocity match, the factors that influenced the transfer alignment were analyzed, such as lever arm effect, flexible vibrations, etc.
通过建立动基座对准速度匹配的系统模型，对影响传递对准的一些重要因素如杆臂效应、挠曲振动等进行了分析，按照既定的载机机动方案采集飞行数据进行离线仿真。
By establishing the system model of moving-base alignment velocity match, the factors that influenced the transfer alignment were analyzed, such as lever arm effect, flexible vibrations, etc.
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