Schmidt-Kalman Filter for Navigation Biases Mitigation during Mars Entry-Reference-Cited by-同舟云学术

Schmidt-Kalman Filter for Navigation Biases Mitigation during Mars Entry

Published:2015-07 Issue:4 Volume:28 Page:04014101
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lou Taishan¹,Fu Huimin²,Wang Zhihua³,Zhang Yongbo³

Affiliation:

1. Ph.D. Student, Research Center of Small Sample Technology, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China (corresponding author).

2. Professor, Research Center of Small Sample Technology, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

3. Lecturer, Research Center of Small Sample Technology, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000423

Reference19 articles.

1. Boehmer R. A. (1998). “Navigation analysis and design for Mars entry.” Ph.D. thesis Massachusetts Institute of Technology Cambridge MA.

2. Mars Exploration Entry, Descent, and Landing Challenges

3. Chu C. C. (2006). “Development of advanced entry descent and landing technologies for future Mars missions.” IEEE Proc. Aerospace Conf. Institute of Electrical and Electronics Engineers New York.

4. Kalman Filtering

5. Levesque J. F. (2006). “Advanced navigation and guidance for high-precision planetary landing on Mars.” Ph.D. thesis Universite de Sherbrooke QC Canada.

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