Optimal Station Keeping for XIPS Thrusters in Failure Mode under Eclipse Constraints-Reference-Cited by-同舟云学术

Optimal Station Keeping for XIPS Thrusters in Failure Mode under Eclipse Constraints

Published:2016-11 Issue:6 Volume:29 Page:04016041
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Jingrui¹,Zhao Shuge²,Zhou Zhicheng³,Li Xingang⁴

Affiliation:

1. Professor, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.

2. Ph.D. Student, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China (corresponding author).

3. Research Fellow, Communications Satellite Division, China Academy of Space Technology, Beijing 100094, China.

4. Senior Engineer, Communications Satellite Division, China Academy of Space Technology, Beijing 100094, 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.1943-5525.0000638

Reference27 articles.

1. Anzel B. (1988). “Controlling a stationary orbit using electric propulsion.” 20th Int. Electric Propulsion Conf. Garmisch-Partenkirchen Federal Republic of Germany 306–314.

2. Anzel B. (1998). “Stationkeeping the Hughes HS 702 satellite with a xenon ion propulsion system.” 49th IAF Int. Astronautical Congress AIAA.

3. Optimal Fuel-Balanced Impulsive Formationkeeping for Perturbed Spacecraft Orbits

4. Berlin P. (1988). “The geostationary applications satellite.” Cambridge University Press Cambridge U.K.

5. Douglas T. Kelly C. and Grisé A. (2004). “On-orbit stationkeeping with ion thrusters Telesat Canada’s bss-702 experience.” SpaceOps Montreal.

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