Abstract
Considering that the spacecraft flying along its fixed elliptical trajectory will easily be tracked and intercepted, a general approach based on jump control input is proposed for the spacecraft anti-tracking model-reference tracking control problem. By combing with the definition of stochastic stability and model-reference tracking, the mathematical description of the spacecraft anti-tracking model-reference tracking control problem is put forward. Based on both stochastic stability theory of jump systems and model reference tracking control method, a feedback controller with stochastic stability and a feedforward controller optimized with free parameters are built. The effectiveness of the proposed control scheme is illustrated by the numerical simulation result of spacecraft anti-tracking.
| Original language | English |
|---|---|
| Pages (from-to) | 684-690 |
| Number of pages | 7 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 36 |
| Issue number | 6 |
| DOIs | |
| State | Published - 30 Jun 2015 |
Keywords
- Model-reference tracking control
- Spacecraft anti-tracking
- Stochastic system
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