Abstract
Satellites formation moving on low earth orbit suffers from the influence of J2 and atmosphere perturbation, then the orbit configuration of the formation will be destroyed in a short time. The relative orbit of the follower satellite with respect to the leader one is described by the mean orbit elements. Under the J2 and atmosphere perturbation, a state equation with the mean elements as the controlled variables is proposed based on Gauss perturbation equation and a nonlinear control law is presented accordingly. In the end, simulation results show the effectiveness of the given controller.
| Original language | English |
|---|---|
| Pages (from-to) | 1327-1330 |
| Number of pages | 4 |
| Journal | Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics |
| Volume | 29 |
| Issue number | 8 |
| State | Published - Aug 2007 |
Keywords
- Atmosphere perturbation
- Mean orbit element
- Nonlinear control
- Satellites formation
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