Orbit optimization of Mars orbiters for entry navigation: From an observability point of view-Reference-Cited by-同舟云学术

Orbit optimization of Mars orbiters for entry navigation: From an observability point of view

Published:2015-06 Issue: Volume:111 Page:136-145
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Yu Zhengshi^ORCID,Zhu Shengying,Cui Pingyuan

Funder

National Basic Research Program of China (973 Program)

National Natural Science Foundation of China

Research Fund for the Doctoral Program of Higher Education of China

Beijing Institute of Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Solar System Exploration;NASA Office of Space Science,2003

2. M. Adler, M. Wright, C. Campbell, I. Clark, W. Engelund, and T. Rivellini, Draft entry, descent and landing Roadmap, NASA Report. TA09, National Aeronautics and Space Administration, Washington, DC, November, 2010.

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

4. Guidance, navigation, and control system performance trades for Mars pinpoint landing;Steinfeldt;J. Spacecr. Rockets,2010

5. A.A. Wolf, C. Graves, R. Powell, and W. Johnson, Systems for pinpoint landing at Mars, in: Proceedings of the 14th AAS/AIAA Space Flight Mechanics Conference, AAS 04-272, Maui, HI, 8–12 February, 2004.

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