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Description: This paper deals with the issue of incorporating pseudolite measurements into an integrated Global Positioning System/
Inertial Navigation System ~GPS/INS! positioning and attitude system with a view to improving signal availability, solution reliability, and
accuracy in a localized area
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Size: 526958 |
Author: huzhou |
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Description: 介绍了单天线GPS姿态定位，希望对大家有帮助-Introduce a single-antenna GPS attitude positioning, in the hope that everyone has to help
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Size: 786432 |
Author: 李冠中 |
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Description: 尽管现在捷联惯导 GPS测向 应用很广泛 测量精度很精确 但不可避免都有自身的缺点，因此再次讨论常规无线电测向测姿问题-Although SINS application of GPS measurements to a wide range of measurement accuracy is very precise but inevitably has its own shortcomings, so once again the discussion of conventional radio direction finder to the attitude determination problem
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Size: 1234944 |
Author: 魏蓝 |
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Description: This paper deals with the issue of incorporating pseudolite measurements into an integrated Global Positioning System/
Inertial Navigation System ~GPS/INS! positioning and attitude system with a view to improving signal availability, solution reliability, and
accuracy in a localized area
Platform: |
Size: 526336 |
Author: huzhou |
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Description: 基于载波相位三差的航天器GPS/INS组合姿态算法-Based on carrier phase III spacecraft poor GPS/INS Attitude Algorithm portfolio
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Size: 765952 |
Author: 陳翔 |
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Description: MEMS与双GPS测姿系统进行组合导航设计-MEMS and dual GPS attitude determination system navigation design
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Size: 172032 |
Author: c |
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Description: 利用gps多天线载波相位技术，确定姿态软件。-The use of multi-antenna gps carrier phase technology, attitude determination software.
Platform: |
Size: 662528 |
Author: yanrui geng |
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Description: An integer ambiguity resolution algorithm for real-time GPS attitude determination
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Size: 847872 |
Author: Vimit Gandhi |
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Description: This project will use the Arduino Diecimila as the hardware platform to control a quadrocopter. Software coding will be done in the Arduino environment. The primary goal for this quadrocopter will be to create a low cost flying vehicle which integrates gyros, accelerometers and a GPS for attitude control compatible with a 2.4GHz RC controller like the Spektrum DX7. A secondary goal would be to make this an autonomous UAV, which can fly to programmed waypoints without pilot intervention.
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Size: 53248 |
Author: marshallab |
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Description: 文针对 INS/ GPS舰船用组合导航系统进行
研究,为提高 INS 误差的修正精度,采用高精度
GPS姿态测量系统为 INS提供外部修正信息,以增
强系统的观测量.在对自适应卡尔曼滤波器分析的
基础上,提出了一种新的基于新息估计的自适应卡
尔曼滤波算法,以解决外部量测噪声出现不确定强
度变化问题.-Text for the INS/GPS navigation system for ships to study, to improve the accuracy of INS error correction, using high-precision GPS attitude measurement system for the INS amended to provide external information to enhance the system of observations. In the adaptive Kalman filter Based on the analysis, a new interest rate is estimated based on the new adaptive Kalman filter algorithm to solve the external uncertainties, the measurement noise intensity change.
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Size: 821248 |
Author: 和平 |
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Description: 基于GPS的实时高动态高精度快速定位定姿算法研究,对不同地点的环境均有很详细的说明。值得一看。-High dynamic GPS-based real-time attitude determination algorithm for high accuracy and fast positioning research on the different locations of the environment are very detailed instructions. Worth a visit.
Platform: |
Size: 290816 |
Author: 烟雨楼 |
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Description: GPS 多天线系统的姿态确定，matlab工具箱-A MATLAB toolbox for attitude determination with GPS multi-antenna systems
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Size: 664576 |
Author: 天笑 |
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Description: 双GPS定向技术应用 载波相位 模糊度解算 寻找方位角 精确度高-Directional technology of dual GPS carrier phase ambiguity resolution azimuth and high accuracy
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Size: 1185792 |
Author: 陈晓明 |
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Description: 研究GPS与INS数据融合编程卡尔曼滤波算法-Study of GPS and INS data fusion programming Kalman filter algorithm
Platform: |
Size: 594944 |
Author: 孙冬凯 |
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Description: 多GPS天线姿态确定程序，包括文件读取、单点定位、双差定位、坐标转换以及姿态确定等。-a MATLAB toolbox for determining the attitude of a rigid platform
by means of multiple non-dedicated antennas using global positioning system is presented.
The programs embedded in this toolbox cover the RINEX data analysis, single point positioning,
differential positioning, coordinate conversion, attitude determination, and other auxiliary functions.
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Size: 657408 |
Author: nemer |
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Description: 多天线姿态确定工具箱，包括星历读取、单点定位、差分定位、坐标转换、定姿等-In this paper a MATLAB toolbox for determining the attitude of a rigid platform by means of multiple non-dedicated antennas using global positioning system is presented. The programs embedded in this toolbox cover the RINEX data analysis, single point positioning, differential positioning, coordinate conversion, attitude determination, and other auxiliary functions. After forming the baselines through double-differenced (carrier phase smoothed) code observables, the attitude parameters are obtained by applying the direct attitude computation and the least squares attitude estimation. The theoretical background is summarized, and some hints regarding the software implementation are given in the paper. Moreover, improvements yielding an expanded functionality are proposed.
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Size: 657408 |
Author: nemer |
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Description: GPS罗盘，GPS罗经仪，GPS定向仪，地平仪，卫星分布图，GPS定向定姿，基于UBLOX LEA-6T-GPS Compass/Attitude Determination
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Size: 634880 |
Author: 陈万通 |
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Description: GPS例程源码，主要讲解的通信方式-Flight control source, mainly on Mpu6050 of communication and attitude solution.
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Size: 66560 |
Author: 马清宗 |
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Description: Linear array using cut than learning laid upon the right control of the main sidelobe ratio, Continuous phase modulation signal (CPM) to produce, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
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Size: 6144 |
Author: dgmsqg
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Description: Including AHP, factor analysis, regression analysis, cluster analysis, Debugging can be used, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle.
Platform: |
Size: 11264 |
Author: yanfengkuiman
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