Multiple spacecraft configuration designs for coordinated flight missions
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[1] Reinhard Diestel,et al. Graph Theory , 1997 .
[2] Byron D. Tapley,et al. Gravity model determination from the GRACE mission , 2008 .
[3] W. H. Clohessy,et al. Terminal Guidance System for Satellite Rendezvous , 2012 .
[4] Gerhard Krieger,et al. TanDEM-X: a TerraSAR-X add-on satellite for single-pass SAR interferometry , 2004, IGARSS 2004. 2004 IEEE International Geoscience and Remote Sensing Symposium.
[5] G. Hill. Researches in the Lunar Theory , 1878 .
[6] K. Yamanaka,et al. New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit , 2002 .
[7] Staffan Persson. B . 07 PRISMA-DEMONSTRATION MISSION FOR ADVANCED RENDEZVOUS AND FORMATION FLYING TECHNOLOGIES AND SENSORS , 2005 .
[8] John L. Junkins,et al. Spacecraft Formation Flying Control using Mean Orbit Elements , 2000 .
[9] Eberhard Gill,et al. Delayed Target Tracking for Along-Track Formations , 2015 .
[10] Dołęga Bogusław. Advances in aerospace guidance, navigation and control : selected papers of the Fourth CEAS Specialist Conference on Guidance, Navigation and Control held in Warsaw, Poland, in April 2017 , 2018 .
[11] Riccardo Bevilacqua,et al. Analytical guidance for spacecraft relative motion under constant thrust using relative orbit elements , 2014 .
[12] Pini Gurfil,et al. Optimal Fuel-Balanced Impulsive Formationkeeping for Perturbed Spacecraft Orbits , 2008 .
[13] Jason J. Westphal,et al. Formation establishment and reconfiguration using differential elements in J2-perturbed orbits , 2014 .
[14] T. Carter,et al. Fuel-Optimal Rendezvous Near a Point in General Keplerian Orbit , 1987 .
[15] Markus Schlotterer,et al. Quasi-impulsive maneuvers to correct mean orbital elements in LEO , 2019 .
[16] Pini Gurfil,et al. Cluster Flight Algorithms for Disaggregated Satellites , 2013 .
[17] O. Montenbruck,et al. Proximity Operations of Formation-Flying Spacecraft Using an Eccentricity/Inclination Vector Separation , 2006 .
[18] David R. Wood,et al. An algorithm for finding a maximum clique in a graph , 1997, Oper. Res. Lett..
[19] R. D. Gibson. Theory and problems of heat transfer, (schaum's outline series): McGraw-Hill, New York (1978) , 1979 .
[20] V. K. Balakrishnan. Schaum's outline of theory and problems of graph theory , 1997 .
[21] Richard Golding,et al. Pleiades Fractionated Space System Architecture and the Future of National Security Space , 2008 .
[22] P. Gurfil,et al. The SAMSON Project – Cluster Flight and Geolocation with Three Autonomous Nano-satellites , 2012 .
[23] Oliver Montenbruck,et al. E/I-vector separation for safe switching of the GRACE formation , 2006 .
[24] David Mishne,et al. Formation Control of Satellites Subject to Drag Variations and J2 Perturbations , 2002 .
[25] Kyle T. Alfriend,et al. Hybrid Cartesian and Orbit Element Feedback Law for Formation Flying Spacecraft , 2000 .
[26] P. Pardalos,et al. An exact algorithm for the maximum clique problem , 1990 .
[27] H. Schaub,et al. J2 Invariant Relative Orbits for Spacecraft Formations , 2001 .
[28] Simone D'Amico,et al. Autonomous Formation Flying in Low Earth Orbit , 2010 .
[29] R. Battin. An introduction to the mathematics and methods of astrodynamics , 1987 .
[30] Jonathan P. How,et al. Spacecraft Formation Flying: Dynamics, Control and Navigation , 2009 .
[31] Pini Gurfil,et al. Closed-loop distance-keeping for long-term satellite cluster flight , 2014 .