Attitude and orbit control systems for the LISA Pathfinder mission-Reference-Cited by-同舟云学术

Attitude and orbit control systems for the LISA Pathfinder mission

Published:2013-01 Issue:1 Volume:24 Page:283-294
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Giulicchi Luisella,Wu Shu-Fan,Fenal Thomas

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference6 articles.

1. L. Giulicchi, T. Fenal, S.-F. Wu, LISA Pathfinder mission, attitude and orbit control based on micro-propulsion systems, AIAA-2009-5997, in: AIAA Guidance, Navigation, and Control Conference, Aug. 2009, Chicago, Illinois, USA.

2. Mission design for LISA Pathfinder;Landgraft;Classical and Quantum Gravity,2005

3. G.D. Racca, P.W. McNamara, The LISA Pathfinder mission: Tracing Einsteinʼs geodesics in space, Space Science Review (Dec. 2009).

4. Spacecraft drag-free attitude control system design with quantitative feedback theory;Wu;Acta Astronautica,2008

5. S.-F. Wu, L. Giulicchi, T. Fenal, M. Watt, Attitude stabilization of LISA Pathfinder spacecraft using colloidal micro-Newton thrusters, AIAA-2010-8198, in: AIAA Guidance, Navigation, and Control Conference, Aug. 2010, Toronto, Ontario, Canada.

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