Research output: Contribution to journal › Article › peer-review
A problem of relative motion of orbiting bodies is investigated on the example of the free motion of any body ejected from the orbital station that stays in a circular orbit around the earth. An elementary approach is illustrated by a simulation computer program and supported by a mathematical treatment based on approximate differential equations of the relative orbital motion.
| Original language | English |
|---|---|
| Pages (from-to) | 63-67 |
| Number of pages | 5 |
| Journal | American Journal of Physics |
| Volume | 69 |
| Issue number | 1 |
| DOIs | |
| State | Published - 1 Jan 2001 |
ID: 51954749