A new landing site uncertainty analysis method for Mars entry mission

Gao Feng Ren*, Sheng Ying Zhu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

4 Citations (Scopus)

Abstract

To evaluate how the uncertain factors in the entry dynamics such as the navigation errors at the entry point affect the landing precision effectively, by introducing the Galerkin projection, a rapid landing error prediction method for Mars entry is proposed. In this method, the Polynomial Chaos are used to approximate the vehicle's states, and the problem is converted to a deterministic dynamical systems. Applying the method to a representative entry scenario of our country's future Mars entry mission, simulation results indicate that, compared with Monte Carlo method, the proposed method is able to predict the mean and covariance with little error and more computational efficiency.

Original languageEnglish
Pages (from-to)14-20
Number of pages7
JournalHarbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology
Volume44
Issue number7
Publication statusPublished - Jul 2012

Keywords

  • Galerkin projection
  • Landing error
  • Mars landing
  • Orthogonal polynomial

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