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On the periodic solutions emerging from the cylindrical precession of an axisymmetric satellite in a circular orbit
Affiliation:1. Institute for Nonlinear Mechanics, University of Stuttgart, Pfaffenwaldring 9, 70569 Stuttgart, Germany;2. Institute of Aircraft Propulsion Systems, University of Stuttgart, Pfaffenwaldring 6, 70569 Stuttgart, Germany;1. Department of Reliability and Dynamic Strength, A. Podgorny Institute of Mechanical Engineering Problems, National Academy of Sciences of Ukraine, 2/10 Dm. Pozharskoho St., 61046 Kharkiv, Ukraine;2. Department of Continuum Mechanics, National Technical University “KhPI”, Frunze St. 21, Kharkiv 61002, Ukraine;1. Department of Mechanical Engineering, University of Bristol, Bristol BS8 1TR, UK;2. School of Engineering, University of Glasgow, Glasgow G12 8QQ, UK;3. Department of Mechanical Engineering, University of Sheffield, Sheffield S1 3JD, UK
Abstract:
Keywords:Periodic solution  Symmetrical satellite  Cylindrical precession  Averaging theory
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