Abstract
A feasible maneuver projects through only one orbit maneuver for rendezvous were studied, Based on the analysis of flight time formula, the general predicted mathematic model of orbital transfer is setup. A method of seeking maneuver point set was presented, and the concept of tracing area was put forward. A great lot of simulations were done to analysis the relation among the tracing-area and some restrictions such as time and fuel, and the simulation results indicate that this method, which is simple and easy to be realized, is reasonable and satisfied under the restrictions of time and fuel.
| Original language | English |
|---|---|
| Pages (from-to) | 1228-1232 |
| Number of pages | 5 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 27 |
| Issue number | 6 |
| State | Published - Nov 2006 |
Keywords
- Orbit maneuver
- Space rendezvous
- Spacecraft
- Tracing area