A comparative study of dynamics models for satellite formation flying - Cartesian ordinary differential equations description
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[1] M. Watkins,et al. GRACE: millimeters and microns in orbit , 2002 .
[2] Eberhard Gill,et al. Tight formation flying for an along-track SAR interferometer , 2003 .
[3] Gerhard Krieger,et al. Interferometric Synthetic Aperture Radar (SAR) Missions Employing Formation Flying , 2010, Proceedings of the IEEE.
[4] Thomas K. Meehan,et al. The Instrument on NASA's GRACE Mission: Augmentation of GPS to Achieve Unprecedented Gravity Field Measurements , 2002 .
[5] Jaime Hueso Gonzalez,et al. TanDEM-X: A satellite formation for high-resolution SAR interferometry , 2007 .
[6] Finn Ankersen,et al. Design and modeling of the formation-flying GNC system for the DARWIN interferometer , 2004, SPIE Astronomical Telescopes + Instrumentation.
[7] Danwei Wang,et al. Comparison study of relative dynamic models for satellite formation flying , 2008, 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics.
[8] Jonathan P. How,et al. Spacecraft Formation Flying: Dynamics, Control and Navigation , 2009 .
[9] R. den Hartog,et al. Darwin: a mission overview , 2006, SPIE Astronomical Telescopes + Instrumentation.