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Innovative Mars entry integrated navigation using modified multiple model adaptive estimation

  • Published:2014-12 Issue: Volume:39 Page:403-413
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Li Shuang,Jiang Xiuqiang,Liu Yufei

Funder

National Natural Science Foundation of China

National High Technology Research and Development Program of China

Qing Lan Project of Jiangsu Province, Innovation Funded Project of Shanghai Aerospace Science and Technology

Fundamental Research Funds for the Central Universities

Foundation of Graduate Innovation Center in NUAA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference33 articles.

1. Navigation analysis and design for Mars entry;Boehmer,1998

2. GN&C technology needed to achieve pinpoint landing accuracy at Mars;Brand,2004

3. Mars exploration entry, descent, and landing challenges;Braun;J. Spacecr. Rockets,2007

4. Expected EDL navigation performance with spacecraft to spacecraft radiometric data;Burkhart,2005

5. Development of advanced entry, descent, and landing technologies for future Mars Missions;Chu,2006

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