搜索资源列表
GPS_DOP
- ％ This program calculates Dilution of Precision with respect to a GPS * ％ receiver given its Cartesian ECEF position and the positions of four or * ％ more visible GPS satellites. It is a validation of the DOP algorit
llhandecefTrans
- 大地坐标（llh）与ECEF直角坐标（xyz）间的转换
GlobalPositioningSystemsInertialNavigationanditegr
- 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, Lawr
GPS_DOP
- ％ This program calculates Dilution of Precision with respect to a GPS * ％ receiver given its Cartesian ECEF position and the positions of four or * ％ more visible GPS satellites. It is a validation of the DOP algorit
llhandecefTrans
- 大地坐标（llh）与ECEF直角坐标（xyz）间的转换-Geodetic coordinates (llh) and the ECEF rectangular coordinates (xyz) to switch between
GlobalPositioningSystemsInertialNavigationanditegr
- 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, Lawr
ecef2eci
- 此matlab函数可以在ECEF和ECI坐标之中转换地点和速率信息。-This matlab function ECEF and ECI can convert the coordinates of the location and rate information.
transformation
- 地球坐标系ecef坐标与地理坐标系(bj54/wgs84)转换。-Ecef coordinate system and geographic coordinates (bj54/wgs84) conversion.
ECEFtoLLA
- Conversion from ECEF to LLA algorithm developed in matlab
lla2ecef
- coordinatetransformation from local to ecef!
ecef2llh_iter
- Function convert the coordinates from ECEF to LLH
alm2pos
- ALM2POS computation for satellite position from almanac data file [pos,R]=alm2pos(almanac,PRN,time) calculates the satellite position in the Terrestial and in the Celestial reference fr a me for a desiderate sate
global_6state_M
- Determine the target s ECEF position based on up to 4 sensor s measurements. The sensor has range, bearing, and elevation data. The measurements were used for Kalman filter processing.-Determine the target s ECEF positio
ECEF_GLS
- 地心地固（ECEF）坐标系下，基于广义最小二乘的雷达组网空间误差配准-Radar network based on generalized least square error of registration space
ECEFtoECI
- Convert WGS 84 (CTS, ECEF) Coordinates to ECI (CIS, Epoch J2000.0) Coordinates. This function has been vectorized for speed. The associated error in converting between coordinate fr a mes is on the order of 1.2*10^-11 km
c
- 导航定位中的坐标转换,从LLA到ECEF的坐标转换-Navigation and positioning of the coordinate conversion from LLA to ECEF Coordinate Transformation
ecef2lla
- Convert geodetic coordinates to Earth-centered Earth-fixed (ECEF) coordinates-Convert [x y z] ECEF [m] vector to [lat lon alt] vector in [rad] and [m]
DCEF
- 最新delphi ECEF控件 ,支持到10.2 tokyo(The latest Delphi ECEF controls, support to 10.2 Tokyo)
ecef+sins
- 代码1用于将位置经纬高信息转换为地心地固坐标系下xyz信息；代码2是捷联惯导算法代码，用于将加速度计和陀螺仪输出的信息进行解算得到位置、速度和姿态信息。(Code 1 is used to convert the location of warp and weft information into XYZ information in a geocentric coordinate system; code 2 is a strapdo