In-orbit calibration of drag-free satellites

Bard, 1974 Bendat, 1998 Chu, 1996, Modified recursive maximum likelihood adaptive filter for nonlinear aircraft, flight-path reconstruction, Journal of Guidance, Control and Dynamics, 19, 10.2514/3.21784 Chu, Q.P. Maximum likelihood parameter identification of flexible spacecraft. Ph.D thesis, Technical University Delft, The Netherlands, 1987. Clemen, C. New method for on-orbit-determination of parameters for guidance, navigation and control, in: Proceedings of the 52nd International Astronautical Congress, Toulouse, France, International Astronautical Federation (IAF), 2001a. Clemen, C. Recherche, Entwicklung und Vergleich von Methoden zur In-Orbit- Bestimmung von Parametern eines Triebwerksystems zur Lageregelung von Satelliten. Master’s thesis, Institut fr Flugmechanik und Raumfahrttechnik, Technical University of Braunschweig, in German, 2001b. Goodwin, 1977 Jafry, Y.R. Aeronomy coexperiments on drag-free satellites with proportional thrusters: GP-B and STEP. Ph.D thesis, Department of Aeronautics and Astronautics of Stanford University, 1992. Krantz, T. Entwicklung und Vergleich von Verfahren zur In-Orbit-Bestimmung des magnetischen Dipolmomentes eines Satelliten. Master’s thesis, Department of Electrical Engineering and Information Technology, University of Bremen, in German, 2002. Lange, B. The control and use of drag-free satellites. Ph.D thesis, Department of Aeronautics and Astronautics of Stanford University, 1964. Ljung, 1999 Nelder, 1965, A simplex method for function minimization, The Computer Journal, 7, 308, 10.1093/comjnl/7.4.308 Theil, S. Satellite and test mass dynamics modeling and observation for drag-free satellite control of the STEP mission. Ph.D thesis, Department of Production Engineering, University of Bremen, 2002. Theil, S., She, H., Schleicher, A. State estimation for drag-free control of the STEP satellite, in: AAS/AIAA Space Flight Mechanics Meeting, San Antonio, TX, 2002. Walters, 1991 Wiktor, P.J. The design of a propulsion system using vent gas from a liquid helium cryogenic system. Ph.D thesis, Department of Aeronautics and Astronautics of Stanford University, 1992. Wright, 1996, Direct search methods: once scorned, now respectable, 191