Abstract
Two-impulse control is used for concomitant orbital control. Based on concomitant motion sate transferring equation, analytic solution of two-impulse concomitant orbital transfer is derived, the control variables are optimized by means of genetic algorithm, and optimal transfer time and trajectories are gained.
| Original language | English |
|---|---|
| Pages (from-to) | 398-400 |
| Number of pages | 3 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 25 |
| Issue number | 4 |
| State | Published - Jul 2004 |
Keywords
- Concomitant orbit
- Concomitant satellite
- Optimization
- Orbital maintenance
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