首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Asymptotic study of a complete magnetic attitude control cycle providing a single-axis orientation
Institution:1. Keldysh Institute of Applied Mathematics of RAS, Miusskaya sq., 4, Moscow 125047, Russia;2. Moscow Aviation Institute, Volokolamskoe Shosse, 4, Moscow 125993, Russia;1. Space Systems Dynamics and Control Laboratory, Dept. of Aerospace Engineering, Ryerson University, M5B 2K3, Toronto, Ontario, Canada;2. PMO, Planet, Berlin, Germany;3. Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur, West Bengal, 721302, India;1. Stanford University, 496 Lomita Mall, Stanford, CA 94305, United States;2. NASA Ames Research Center, Moffett Field, CA 94035, United States;3. Millennium Engineering and Integration Services, 2231 Crystal Dr, Arlington, VA 22202, United States;4. University of Michigan, 1320 Beal Ave, Ann Arbor, MI 48109, United States;1. Instituto de Matemática e Estatística, Universidade Federal Fluminense, Niterói, RJ, Brazil;2. Institute of Optimization and Operations Research, Ulm University, Ulm, Germany
Abstract:The angular motion of an axisymmetrical satellite equipped with the active magnetic attitude control system is examined. Attitude control system has to ensure necessary orientation of the axis of symmetry in the inertial space. It implements the following strategy: coarse reorientation of the axis of symmetry with nutation damping or “-Bdot” without initial detumbling; spinning-up about the axis of symmetry to achieve the property of a gyro; fine reorientation of the axis in the inertial space. Dynamics of the satellite is analytically studied using averaging technique on the complete control loop consisting of five algorithms. Solutions of the equations of motion are obtained in terms of quadratures for most cases or even in closed-form. The latter allowed to study the dependence of motion parameters including time-response with respect to the orbit inclination and other parameters for all algorithms.
Keywords:
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号