Abstract
Two clusters of formation flying satellites with a relative angle on geosynchronous Earth orbit were used to construct a space-based continuous navigation system for deep space exploration. Adopting technique of passive navigation by multiple base-stations, formation flying satellites obtained high precision of navigation according to time and frequency difference of arrival of downlink signal from deep space explorer. Enhancing system timing and carrier frequency, and increasing the length of baselines help to improve precision of navigation. The precision of this navigation system is close to that of NASA's VLBI system.
| Original language | English |
|---|---|
| Pages (from-to) | 1185-1189 |
| Number of pages | 5 |
| Journal | Acta Astronautica |
| Volume | 65 |
| Issue number | 9-10 |
| DOIs | |
| State | Published - Nov 2009 |
| Externally published | Yes |
Keywords
- Continuous navigation
- Deep space exploration
- Formation flying satellite
- Geostationary Earth orbit
- Space-based
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