Astronomy
Rendezvous in a moving frame
Give a nearby spacecraft a radial offset and an along-track impulse. Watch the curved relative path and find a closed formation orbit.

The model and its limits
Linear Clohessy–Wiltshire motion around a circular 400 km orbit. Valid only for small separations; no contact, docking controller or attitude dynamics.
Equations used in the module
Equations x = (4-3cos nt)x₀ + 2(1-cos nt)vy₀/n; y = 6(sin nt-nt)x₀ + (4sin nt-3nt)vy₀/n


