摘要
A method for designing stochastically optimized guidance law is proposed for the adverse effect of estimation error on guidance accuracy. The estimated navigation performance is introduced into the process of guidance design as an optimization term, and the estimation accuracy of visual navigation is improved by optimizing the observation trajectory, thus improving the guidance performance. Furthermore, to avoid iterative computations, the idea of one-step-ahead (OSA) optimization is introduced as a suboptimal strategy. Numerical simulations have demonstrated the effectiveness of the approach proposed.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 1884-1889 |
| 页数 | 6 |
| 期刊 | Yuhang Xuebao/Journal of Astronautics |
| 卷 | 32 |
| 期 | 9 |
| DOI | |
| 出版状态 | 已出版 - 9月 2011 |
指纹
探究 'Stochastically optimized guidance law design of the deep space lander' 的科研主题。它们共同构成独一无二的指纹。引用此
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