The Effectiveness of Solution Technique on the Autonomous Orbit Determination Accuracy of Lagrangian Navigation Constellation
Author:
Affiliation:
1. College of Astronautics, Nanjing University of Aeronautics and Astronautics
2. College of Astronomy and Space Science, Nanjing University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/16/5/16_398/_pdf
Reference17 articles.
1. 1) Farquhar, R. W.: Lunar Communications with Libration-Point Satellites, J. Spacecraft Rockets, 4 (1967), pp. 1383-1384.
2. 2) Hill, K. A.: Autonomous Navigation in Libration Point Orbits, Ph.D. Thesis, University of Colorado, 2007.
3. 3) Grebow, D.: Generating Periodic Orbits in the Circular Restricted Three-Body Problem with Applications to Lunar South Pole Coverage, M.S. Thesis, Purdue University, 2006.
4. 4) Romagnoli, D. and Circi, C.: Lissajous Trajectories for Lunar Global Positioning and Communication Systems, Celest Mech Dyn Astr, 107 (2010), pp. 409-425.
5. 5) Circi, C., Romagnoli, D. and Fumenti, F.: Halo Orbit Dynamics and Properties for a Lunar Global Positioning System Design, Monthly Notices of the Royal Astronomical Society, 442 (2014), pp. 3511-3527.
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