Abstract
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.
Original language | English |
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Pages (from-to) | 1884-1889 |
Number of pages | 6 |
Journal | Yuhang Xuebao/Journal of Astronautics |
Volume | 32 |
Issue number | 9 |
DOIs | |
Publication status | Published - Sept 2011 |
Keywords
- Deep space exploration
- Navigation and guidance system
- One-step-ahead approach
- Optimal estimated
- Soft landing
- Stochastic optimization algorithm