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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, Lawrence Weill, and A. P. Andrews,
ECEFtoLLA
- Conversion from ECEF to LLA algorithm developed in matlab
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 position based on up to 4 sensor s me
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 frames is on the order of 1.2*10^-11 km when compared to STK ephemeris
zuobiaoxizhuanhuan
- GPS中ECEF\LLW\ECI等坐标系的转换，为matlab程序，已打包-GPS ecef,eci,llw...
ECEF-LLT
- Matlab子程序，实现直角坐标系-大地坐标系-站心坐标系的转换。-Matlab subroutine achieve Cartesian coordinates- geodetic coordinate system- topocentric coordinate system conversion.
XYZtoGPS
- converts ECEF XYZ coordinates to ECEF lla ( latitude, longitude, altitude) in WGS84. matlab