Stochastically optimized guidance law design of the deep space lander

Ai Gao*, Ping Yuan Cui, Hu Tao Cui

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

5 Citations (Scopus)

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 languageEnglish
Pages (from-to)1884-1889
Number of pages6
JournalYuhang Xuebao/Journal of Astronautics
Volume32
Issue number9
DOIs
Publication statusPublished - Sept 2011

Keywords

  • Deep space exploration
  • Navigation and guidance system
  • One-step-ahead approach
  • Optimal estimated
  • Soft landing
  • Stochastic optimization algorithm

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