Abstract
The paper presents how the formation is controlled to the intended shape by a decentralized control. The formation behaviour is dealt via a z-transformation method and a uniformly convergent strategy that each spacecraft performs is proposed. Not only one-dimensional but tow-dimensional examples are shown. Since the strategy is highly flexible, it is applicable to a variety of the formation flying space missions.
| Original language | English |
|---|---|
| Pages (from-to) | 417-422 |
| Number of pages | 6 |
| Journal | European Space Agency, (Special Publication) ESA SP |
| Issue number | 548 |
| Publication status | Published - 2004 |
| Externally published | Yes |
| Event | 18th International Symposium on Space Flight Dynamics - Munich, Germany Duration: 11 Oct 2004 → 15 Oct 2004 |