Description: 这是本人用SIMLINK辨析的一个用经典控制理论方法实现的接联惯性导航系统精对准的方法程序。-using SIMLINK Analysis with the use of a classical control theory method of access inertial navigation systems EC precision alignment methods and procedures. Platform: |
Size: 6155 |
Author:吉庆昌 |
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Description: 这是本人用SIMLINK辨析的一个用经典控制理论方法实现的接联惯性导航系统精对准的方法程序。-using SIMLINK Analysis with the use of a classical control theory method of access inertial navigation systems EC precision alignment methods and procedures. Platform: |
Size: 6144 |
Author:吉庆昌 |
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Description: 在捷联式惯性导航系统中，惯性敏感器直接固联在载体上，惯性敏感器的工作条件和环境与单独测试惯性敏感器时有较大的差别。并且当惯性敏感器安装到惯性组件上以后，还存在各种安装误差，因此对惯性敏感器单独测试的结果并不能反映惯性敏感器在系统中实际的
性能品质。为了保证系统的技术性能，现代捷联惯性导航系统均采取了较为全面的误差补偿
措施。捷联惯性导航系统误差补偿的前提则是对惯性组件进行精确的误差标定。
-In strapdown inertial navigation systems, inertial sensors is in direct solid carriers, inertial sensors, working conditions and environment with a separate test inertial sensors greater difference. And when the inertial sensor installed after inertial components, there is a variety of installation errors of inertial sensor test results alone do not reflect the inertial sensor in the system, the actual quality performance. In order to ensure the system Platform: |
Size: 248832 |
Author:申亮 |
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Description: This diskette (version 1.0) contains demonstration programs and source codes in MATLAB (v.5.2) for algorithms listed in the textbook Global Positioning Systems, Inertial Navigation, and Integration, by M. S. Grewal, Lawrence Weill, and A. P. Andrews, published by John Wiley and Sons, 2000.
Contents: MATLAB (Version 5.2) Demonstrations & Scripts
Chapter4
ephemeris.m calculates the GPS satellite position in ECEF coordinates from its ephemeris parameters.
Chapter5
Klobuchar_fix.m calculates the ionospheric delay.
Chapter6 (shows the quaternion utilities) -This diskette (version 1.0) contains demonstration programs and source codes in MATLAB (v.5.2) for algorithms listed in the textbook Global Positioning Systems, Inertial Navigation, and Integration, by MS Grewal, Lawrence Weill, and AP Andrews, published by John Wiley and Sons, 2000.Contents: MATLAB (Version 5.2) Demonstrations Platform: |
Size: 12288 |
Author:gaoxu |
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Description: Global Positioning Systems Inertial Navigation and Integration 2nd Edition Wiley Jan 2007 ，经典的GPS与INS组合导航的书-Global Positioning Systems Inertial Navigation and Integration 2nd Edition Wiley Jan 2007, the classic combination of GPS and INS navigation books Platform: |
Size: 3557376 |
Author:sayyou |
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Description: Missing file from "Global Positioning Systems, Inertial Navigation, and Integration" by Mohinder S Grewal, Lawrence R Weill, and Angus P Andrews Platform: |
Size: 3072 |
Author:Sal |
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Description: This book constitutes an excellent source for understanding the basic operation of the Global Positioning Systems (GPS). It also allows the reader to take the first steps towards understanding how the Kalman Filter is implemented in the estimation of drifting parameters of the GPS. The "Kalman Filter Basics" chapter is preceded by a description of the different errors that affect the GPS signals. Furthermore, this book includes sections on the Wide-Area Augmentation System, Inertial Navigation, and Differential GPS, which enables the understanding of these concepts and thus, provides the reader an overall perspective of the Global Positioning System. Platform: |
Size: 3961856 |
Author:anna |
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Description: This publication is designed to provide accurate and authoritative information in regard navigation. Platform: |
Size: 4017152 |
Author:Florin |
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Description: 采用程序的方法介绍捷联惯性导航系统进行导航的方法，并将载体的导航信息输出以检验捷联惯性导航系统的导航效果。-Strapdown inertial navigation systems is a kind of common navigation systems in land vehicles. Platform: |
Size: 5618688 |
Author:约翰肯尼迪 |
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Description: 机载导弹捷联惯性导航系统，空中动基座传递对准技术研究，研究弹载子系统与机载主惯性导航系统在飞行过程中的动态传递对准技术-Airborne missile strapdown inertial navigation systems, air Moving Base Transfer the main alignment technology, research onboard subsystems and airborne inertial navigation system during the flight dynamic Transfer Alignment Platform: |
Size: 1597440 |
Author:赵 |
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Description: 惯导系统轨迹生成器，能生成不同位置转动和舰船摇摆条件下的陀螺和加速度计数据，用于研究惯导系统-INS trajectory generator can generate different locations and ships swing conditions rotating gyroscope and accelerometer data, inertial navigation systems for research Platform: |
Size: 1084416 |
Author:吴修振 |
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Description: 利用因子图和积算法设计的无人机惯性导航系统算法，利用matlab仿真实现(An algorithm of unmanned aerial vehicle (UAV) inertial navigation system designed by factor diagram and calculation method is realized by MATLAB simulation) Platform: |
Size: 1217536 |
Author:峰峰
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