MATLAB EM Algorithm Implementation for Data Clustering
A MATLAB implementation of the EM algorithm for clustering tasks with optimized computational efficiency, featuring clear code structure and practical applications
Kernel-Based Correlation Filter Tracking Method
A cutting-edge kernel-based correlation filter tracking approach from the latest TPMAI publication, featuring exceptionally fast processing speeds with enhanced algorithm implementation details.
Random Forest Algorithm MATLAB Implementation
MATLAB implementation of the Random Forest algorithm providing reliable classification capabilities with comprehensive functionality, though execution speed may be slower compared to optimized implementations
Extracting Invariant Moment Output Results from Images
This MATLAB program extracts invariant moment output results from images, specifically computing the seven classical invariant moments with high processing speed and efficiency.
MFAC Control for Tracking Permanent Magnet Linear Motors
MFAC control implementation for permanent magnet linear motors with velocity and position tracking capabilities using model-free adaptive algorithms
Random Walk Simulation for Information Propagation Speed
A random walk simulation program modeling information transmission speed, presented as a research paper with result visualization graphs and original paper documentation. The implementation includes path generation algorithms, velocity parameters, and source-target coordination mechanisms.
Calculating Satellite Velocity in Earth-Centered Earth-Fixed Frame Using 15 Ephemeris Parameters
Computation of satellite velocity and position in Earth-Centered Earth-Fixed (ECEF) coordinates using 15 ephemeris parameters, including 6 Keplerian orbital elements and 9 perturbation parameters
Satellite Orbital Parameter Acquisition
Deriving satellite orbital parameters from position and velocity vectors
Solving the Lambert Problem
This function solves the Lambert orbital boundary value problem by determining the velocity vectors at two specified position vectors given the transfer time between them. The implementation handles both short-way and long-way trajectories with numerical iteration methods to compute orbital parameters, though the approach may produce high delta-v requirements.