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Autonomous optical navigation algorithm for small body impact mission

  • Ning Du*
  • , Chen Sheng Cai
  • , Hu Tao Cui
  • *Corresponding author for this work
  • Shanghai Aerospace Control Engineering Institute

Research output: Contribution to journalArticlepeer-review

Abstract

Aiming at the high precision requirement of the orbit determination system, an autonomous optical navigation strategy based on B-plane coordinate system was investigated for a small-body impact mission, in which the angle between the target-relative position and velocity vectors could be ignored. The algorithm used images of the target body to update target relative state information. This involved using the object center-of-figure data as the observations and then processing the data through a Kalman filter to update the impactor position and attitude components in the B-plane coordinate. Monte Carlo simulations demonstrate the feasibility of the approach, including the numerical accuracy and stability.

Original languageEnglish
Pages (from-to)1979-1982
Number of pages4
JournalXitong Fangzhen Xuebao / Journal of System Simulation
Volume21
Issue number7
StatePublished - 5 Apr 2009

Keywords

  • Attitude estimation
  • Autonomous optical navigation
  • Kalman filter
  • Small body impact

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