Multi-Satellite Reconfiguration of Formation around Libration Point

Author:

GONG Shengping1,BAOYIN Hexi1,LI Junfeng1

Affiliation:

1. Tsinghua University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference14 articles.

1. 1) Farquhar, R. W.: The Utilization of Halo Orbits in Advanced Lunar Operations [M]. Technical Report TN D-6365, NASA, 1971.

2. 2) Gomez, G., Jorba, A., Masdemont, J. J. and Simo, C.: Study of the Transfer from the Earth to a Halo Orbit around the Equlibrium Point L1, Celestial Mechanics and Dynamical Astronomy, 156 (1993), pp. 541–562.

3. 3) Barden, B. T. and Howell, K. C.: Formation Flying in the Vicinity of Libration Point Orbits Spaceflight Mechanics 1998, Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, Monterey, 1998, pp. 969–988.

4. 4) Howell, K. C. and Marchand, B. G.: Control Strategies for Formation Flight in the Vicinity of the Libration Points, Adv. Astronaut. Sci., 114 (2003), pp. 197–230.

5. 5) Howell, K. C. and Marchand, B. G.: Trajectory Design and Stationkeeping for Multiple Spacecraft in Formation Near the Sun-Earth L1 Point, 50th International Astronautical Congress, Amsterdam, Netherlands, 1999.

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1. Control of orientation for spacecraft formations in the vicinity of the Sun-Earth L2 libration point;Science China Physics, Mechanics & Astronomy;2014-04-24

2. Orbit control strategy for Lagrange point orbits based on an analytical method;Science China Physics, Mechanics and Astronomy;2013-03-08

3. Venus round trip using solar sail;Science China Physics, Mechanics and Astronomy;2012-06-25

4. Multi-modes control method for spacecraft formation establishment and reconfiguration near the libration points;Theoretical and Applied Mechanics Letters;2012

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