Explore MATLAB source code curated for "坐标转换" with clean implementations, documentation, and examples.
This program implements relative orientation, absolute orientation, and 7-parameter coordinate transformation for remote sensing data processing, featuring representative algorithms and practical applicability for trial use.
MATLAB implementation for coordinate conversion from ENU (East-North-Up) frame to ECEF (Earth-Centered Earth-Fixed) system with supporting documentation. The main function ENVtoECEF takes ENU origin latitude/longitude coordinates and ENU point data as input parameters, and outputs corresponding latitude, longitude, and altitude (LLA) coordinates. The implementation includes WGS-84 ellipsoid parameters and transformation algorithms for precise geospatial calculations.
Coordinate Transformation: Determines transformation relationship between two coordinate systems A and B using optimization methods with standard 7-parameter transformation (translation along x,y,z; rotation about x,y,z axes; and scaling factor). Includes spatial rotation formulas. Input: point coordinates in systems A and B. Output: transformation parameters (u,v,w: translation along x,y,z; α,β,γ: rotation angles about x,y,z axes; k: scaling factor).
Implementation of satellite position computation, user position calculation using least squares method, navigation message reading, and coordinate transformation through MATLAB programs.
GPS simulation MATLAB software featuring coordinate transformation, pseudorange calculation, error analysis, and related algorithmic implementations
This comprehensive coordinate transformation tool supports mutual conversions between WGS84, NEU, and rectangular geodetic coordinate systems, featuring extensive testing and optimization for reliable performance.
Coordinate transformation between two coordinate systems, including mathematical algorithms and implementation approaches.
Bidirectional Conversion Between Geocentric Coordinate System and Latitude-Longitude Coordinate System
Essential functions for spacecraft orbit computation including coordinate transformations, latitude-longitude conversions, two-body motion calculations, and orbital element computations with implementation details
GPS Simulation Implementation using MATLAB Code with Coordinate Transformation, Pseudorange Calculation, and Error Analysis