This app is based on Clohessy-Wiltshiere (hill's) equation, which expresses relative dynavmics at relatively close range on circular orbit.
Therefore, there is no other perturbation other than Earth's gravity.
This app support V&R approach (V-bar, R-bar), Glide slope approach, and Circumnavigation.
also you can plan a mission with these combination. If so, it calculates velocity and time.
引用格式
DONGWOO HAN (2026). Rendezvous & Docking Simulation (https://ww2.mathworks.cn/matlabcentral/fileexchange/120318-rendezvous-docking-simulation), MATLAB Central File Exchange. 检索时间: .
MATLAB 版本兼容性
创建方式
R2022a
兼容任何版本