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GPSnavigation.rar
- 这个是关于GPS和捷联惯性导航系统的组合导航技术研究论文,非常有参考价值.,This is about GPS and strapdown inertial navigation system, a combination of navigation technology research papers, a very good reference material.
INS_OUT2
- 捷联惯性导航技术中使用四元数算法实现姿态更新矩阵的求解，得到姿态角。-Strapdown inertial navigation technology using quaternion attitude update algorithm for solving the matrix, get attitude angle.
Strapdown_Inertial_Navigation_Technology
- E-book Strapdown_Inertial_Navigation_Technology
Strapdown
- 《Strapdown inertial navigation technology》全面系统地介绍了捷联惯导的基本原理与计算。-Strapdown inertial navigation technology， a comprehensive and systematic introduction to the basic principles of strapdown inertial navigation system and calculation.
strapdown_navigation_technology
- 捷联惯性导航技术,经典电子书 Strapdown navigation technology 中文版-Inertial navigation technology, the classic book Strapdown Inertial Navigation Technology David H. Titterton Jobn L. Weston Chinese
Strapdown_Inertial_Navigation_Technology
- Strapdown Inertial Navigation Technology. Second Edition.
Cascade-inertial-navigation
- 捷联式惯性导航也就是将惯性测量元件（陀螺仪和加速度计）直接装在飞行器、舰艇、导弹等需要诸如姿态、速度、航向等导航信息的主体上，用计算机把测量信号变换为导航参数的一种导航技术-Strapdown inertial navigation and inertial measuring element is (gyroscope and accelerometer) directly on the aircraft, warships, missiles and other needs such as
DirectionCosin
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准方向余弦法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard method of direction cosine
RotationVector
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准旋转矢量法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard rotation vector method to s
Euler
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准欧拉法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard eulerian method to solve the
捷联惯导及其组合导航研究
- 本文对捷联惯导系统(sINS)及其与全球定位系统(GPS)的组合导航系统进行 了研究。首先对实现S取S的初始对准及姿态矩阵计算等关键技术进行了系统研究。 在仿真的基础上进行了实际捷联惯导系统的系统研制，针对陀螺漂移补偿等关键算法 开展深入研究，实验结果表明经过补偿解算后，整个捷联惯导系统导航参数的解算精 度大大提高。在实现SINS的基础土，研究了SINS与GPS(The strapdown inertial navigation system (sINS) and global posi
daohangthree
- 西工大研一惯性测量实验的粗对准程序以及图示，参考《捷联惯导算法与组合导航原理讲义》(Coarse alignment procedure and graphics for the INS experiment of Xigong University of Technology, refer to the Lecture on Strapdown Inertial Navigation Algorithms and Integrated Navigation Principles.)
捷联惯导算法与组合导航原理讲义(20190410)
- 本书是作者在总结多年研究生“卡尔曼滤波与组合导航原理”课程的教学经验，吸收十余年从事惯性导航与组合导航技术研究的科研成果，以及参阅国内外众多文献资料的基础上编写的，注重基础理论与工程实践相结合，实用性与可操作性强。全书共八章，主要包括捷联惯导算法及其误差分析、地球重力场基础、卡尔曼滤波基本原理、初始对准与组合导航技术、捷联惯导与组合导航仿真等内容。书中附有丰富的Matlab仿真程序可供参考，还有练习题可供读者拓展学习或学生练习使用。(In this book the author summari