Finally the technical scheme of distributed attitude reference is approached.
最后，探讨了分布式姿态基准系统的技术方案。
Theoretic and experiment study of a shipboard attitude reference system using laser gyros.
某船载激光陀螺姿态参考系统的理论分析与实验研究。
The identification of the undetermined parameter in the inertial surveying and attitude reference system.
惯性测量与姿态参考系统中未知参数辨识。
Then the unite attitude reference system of the whole ship is built based on the information fusion on the radial basis function neural networks.
然后基于径向基函数神经网络的信息融合技术建立全舰统一姿态基准系统。
A new design method of compensation loop for the stabilized gyrocompass, as a ship attitude reference, is derived by using modern control theory.
本文利用现代控制理论的方法对舰船姿态基准——平台罗经的修正回路进行了讨论。
The laser gyro inertial surveying and attitude reference system model with incomplete inertial sensors are first derived under the body dynamic constraint.
首次推导了非完整惯性传感器配置条件下，基于载体动态约束的激光陀螺惯性测量与姿态参考模型。
Two aspects of applications of the body dynamic constraint are analyzed as follows: 1 the inertial surveying and attitude reference system with incomplete inertial sensors.
作为新的信息源，论文分析了载体动态约束的两方面应用：1非完整惯性传感器惯性测量与姿态参考系统。
Many references show that the theoretic and practical researches on inertial surveying and attitude reference systems are predominantly in the field of sensor data integration.
文献分析表明，惯性测量与姿态参考系统的理论及应用研究主要集中在传感器信息综合方面。
The LCR-100 Gyrocompass AHRS is a north finding attitude and heading reference system based on a state-of-the-art fibre-optic gyro and micro-electromechanical (MEMS) accelerometers.
LCR- 100罗经ahrs系统是寻北姿态航向参考系统，基于最先进的光纤陀螺和微机电(MEMS)加速度计。
This kind of method describes the position and attitude of objects by utilizing Cartesian coordinates of reference base points and Cartesian components of reference base vector.
这种方法是利用参考基点的笛卡尔坐标和参考基矢量的笛卡尔分量描述物体的位置与姿态。
The neural network adaptive attitude control system is designed based on model reference adaptive control theory and combination of online neural network with augmented model inversion.
首先根据模型参考自适应控制理论，将模型逆与在线神经网络结合，设计了神经网络自适应姿态控制系统。
An adaptive neural network attitude control system is designed based on model reference adaptive control theory and combination of online neural network with augmented model inversion in this paper.
本文根据模型参考自适应控制理论，将旋转动力学逆与在线神经网络结合，设计了自适应姿态控制系统。
Target simulators are used to simulate the environment character of reference objects (the sun, the earth and stars) as satellite attitude sensors.
目标模拟器用来模拟作为卫星姿态敏感器的参考目标(太阳、地球和恒星等)的环境特性。
Abstract: an integrated micro attitude heading reference system (MAHRS) was researched for micro aerial vehicles (MAV) based on the MEMS gyroscopes, accelerometers, and magnetic-sensors.
摘要：研究了基于硅mems陀螺、加速度计及磁阻式磁强计组合的微小型飞行器用姿态航向参考系统。
An integrated micro attitude heading reference system (MAHRS) was researched for micro aerial vehicles (MAV) based on the MEMS gyroscopes, accelerometers, and magnetic-sensors.
研究了基于硅mems陀螺、加速度计及磁阻式磁强计组合的微小型飞行器用姿态航向参考系统。
The measurement error of vehicle's attitude caused by the drift of platform reference is also analyzed.
对由于惯性基准的漂移而引起的载体姿态角的测量误差也进行了分析。
An extended Kalman filter with adaptive gain was used to build a miniature attitude and heading reference system based on stochastic model.
利用改进的自适应增益卡尔曼滤波器在随机模式下建立一个小型姿态确定系统。
To further reduce calculation cost, multiple computing cycles were defined. The output reference attitude command was used to realize the attitude tracking control of reference attitude trajectory.
为进一步降低算法耗费，定义了计算周期的多个层次，最终给出实时参考姿态指令，用以实现参考轨迹的姿态跟踪控制。
Inspired by Yang Xianjiang's conception of "all-life guidance", here we put forth 3 approaches, namely solving concrete problems, providing frame of reference and strengthening the ethical attitude.
本文根据杨贤江“全人生指导”思想的启发，提出了增强德育课实效性的三种手段，即解决具体问题、提供参照构架和强化道德态度。
Moreover, the reference attitude command must be imported from out of the control loop, considering the constraint to attitude sensors selection due to deep-space environment.
同时深空环境对姿态敏感器选用造成了限制，使得从控制回路外部引入参考姿态指令成为必然。
The attitude coordination control problem for formation flying satellites associated with time-varying reference attitude tracking subject to control input saturation is investigated in this paper.
本文研究了跟踪时变参考姿态情况下的控制输入饱和的编队飞行卫星姿态协同控制问题。
This approach has an advantage that requires no reference points and is independent of satellite attitude knowledge or control.
此方法的优点是不需要在星载sar的视场中使用任何位置确知的参考点，并且与卫星的姿态数据无关。
A nonlinear attitude control system was designed by choosing a nonlinear system tracing a linear reference model system, based on model reference variable structure control method.
设计出非线性系统跟踪线性参考模型系统的新的模型参考的变结构控制系统。
It is a scientific attitude towards the construction of a system to compare the different public personnel administrative systems of different countries and use them for reference.
对各国公共人事管理体制进行分析比较，学习借鉴，应是制度建设之科学态度。
Some key techniques, such as attitude correction, quality control of GPS height, transformation of vertical reference datum and extraction of tidal level, are studied in detail.
这些关键问题主要有姿态改正、GPS高程质量控制、垂直基准转换、基于信号的在航潮位提取。
With this measured data, information fusion algorithm is able to design a high precision Attitude and Heading Reference system. Therefore it can accord with the control system demand.
依据这些原始数据设计适当的信息融合算法可以构建高精度的姿态航向参考系统，从而满足控制系统的要求。
The value of reference lies in the three fields: the setting of goal, behavioral habits and the attitude toward work.
老子思想强调的“道”与“无”对青少年的成才成长有重要的借鉴价值，这种借鉴价值主要体现在目标制定、行为习惯、工作态度三个方面。
A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with Strapdown Inertial Navigation System (SINS) as mid-course guidance.
论文针对使用捷联惯导系统为中制导的近距空空导弹，设计了一种基于数字信号处理器(dsp)的小型数字式捷联航姿应用系统。
To improve the accuracy and reduce the setting time for the initial alignment of marine attitude heading reference system(AHRS) under motion, a method of two-position alignment was presented.
为提高船用航姿系统的对准精度和对准速度，提出了摇摆条件下的两位置对准方案。
The attitude feedback processed by a filter was used to adjust continuously the parameters of the reference point, and the lean along the longitudinal and lateral direction are compensated.
采用经滤波处理的姿态反馈角度对中位点各参数进行连续调节，实现过渡状态下对姿态在纵向和横向上的倾斜补偿。
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