Abstract
Under the background of mission on laser communication by formation flying satellites and the assumption of known relative position and attitude, a fully decentralized variable structure relative attitude coordination control strategy with the proof of global stability using a Lyapunov function was given. Simulation results indicate that the proposed method can minimize relative attitude error in the presence of disturbance acting on the satellites in the formation, achieve attitude coordination among the satellites and demonstrate validity of this control strategy.
| Original language | English |
|---|---|
| Pages (from-to) | 1465-1470 |
| Number of pages | 6 |
| Journal | Jilin Daxue Xuebao (Gongxueban)/Journal of Jilin University (Engineering and Technology Edition) |
| Volume | 37 |
| Issue number | 6 |
| State | Published - Nov 2007 |
Keywords
- Control and navigation technology of aerocraft
- Coordination strategy
- Formation flying
- Laser communication
- Relative attitude control
- Variable structure
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