Abstract
The laboratory facility named LuVeX is developed for motion control algorithms verification of the formation flying purposed for the Earth remote sensing. The mock-up description, the parameter determination of its individual elements, description of the realized algorithms for its thruster engine control are given in the chapter. The mathematical simulation results of a mock-up motion controlled with the algorithms which provide the required mock-up formation motion in given trajectories are presented. Several configurations of the formation and formation’s elements coupling methods are shown. Required motion precision and its dependence on formation parameters are examined.
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S. Theil, R. Stanislowski, A. Schleicher, S. Scheidhauer. Entwurf und Entwicklung eines Luftkissenfahrzeugs für einen Satellitendynamiksimulator / Projektbericht, Universität Bremen, Bremen, 2003, 38p.
D. Ivanov, Т. Walter, D. Bindel, M. Ovchinnikov. Laboratory Facility to Verify Motion Control Algorithms for Multi-element Systems, Preprint of KIAM RAS, M.: 2008, N 56, 32p. (http://www.keldysh.ru/papers/2008/prep56/ prep2008_56.html)
D. Ivanov, M. Ovchinnikov. Determination of the Orientation of a Suspended Mock-up Using One-Axis Gyroscope, Preprint of KIAM RAS, Moscow, 2008, N 11, 32p. (http://www.keldysh.ru/papers/2008/prep11/prep2008_11.html)
C. Mehlen, C. Peyrotte, S. Furlan, N. Wilhelm, R. Frenkiel, N. Perriault, L. Pirson, M. Sghedoni. RF Metrology and Data-link Instrument for Formation-flying Missions, Paper on 30th Annual AAS Guidance and Control Conference, AAS 07-067, pp. 567–583.
C. Kuehl, M. Mehl, H. Diehl, E. Gottzein. Micro-Tech.-Sensor for Attitude and Orbit Determination, Paper on 26th Annual AAS Guidance and Control Conference, AAS 03-001, pp. 1–18.
F.P. Vasilyev. Numerical Methods for Extremal Tasks Solving, Moscow. Nauka, 1988, 552p.
M. Ovchinnikov, A. Ilyin, N. Kupriynova, V. Penkov, A. Selivanov. Attitude dynamics of the first Russian nanosatellite TNS-0, Acta Astronautica, 2007, Vol. 61, Issue 1–6, pp. 277–285.
I. Zaramenskikh, M. Ovchinnikov, I. Ritus. Nullifying feasibility of Slow Gravitational Perturbation Effect on the Formation Flying Configuration, Paper on 5th IAA Workshop on Constellations and Formation Flying, Evpatoria, Ukraina, 1–4 July, 2008, 16p.
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Ivanov, D., Ming, Z., Walter, T., Zaramenskikh, I. (2010). Laboratory Facility for Simulation and Verification of Formation Motion Control Algorithms. In: Sandau, R., Roeser, HP., Valenzuela, A. (eds) Small Satellite Missions for Earth Observation. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-03501-2_25
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DOI: https://doi.org/10.1007/978-3-642-03501-2_25
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