Magnetic Attitude Control of a Flexible Satellite

1 M.A.Sc. Candidate, University of Toronto Institute for Aerospace Studies, 4925 Dufferin Street, Toronto, Ontario, Canada, M3H 5T6, and Student Member AIAA. 2 Assistant Professor, Ryerson University, Department of Aerospace Engineering, 350 Victoria Street, Toronto, ON, Canada, M5B 2K3, and Senior Member AIAA. 3 Assistant Professor, McGill University, Department of Mechanical Engineering and Centre for Intelligent Machines, 817 Sherbrooke Street West, Montreal, QC, Canada, H3A 0C3, and Member AIAA. 4 Associate Professor, University of Toronto Institute for Aerospace Studies, 4925 Dufferin Street, Toronto, Ontario, Canada, M3H 5T6, and Senior Member AIAA. 5 Professor, University of Toronto Institute for Aerospace Studies, 4925 Dufferin Street, Toronto, Ontario, Canada, M3H 5T6, and Associate Fellow AIAA. 6 Research Scientist, Canadian Space Agency, Space Science and Technology, 6767 route de l’Aeroport, St.Hubert,QC, J3Y 8Y9, and AIAA member.

[1]  Carlo Arduini,et al.  Active Magnetic Damping Attitude Control for Gravity Gradient Stabilized Spacecraft , 1997 .

[2]  Warren P. Seering,et al.  Preshaping Command Inputs to Reduce System Vibration , 1990 .

[3]  Rafal Wisniewski Linear Time-Varying Approach to Satellite Attitude Control Using Only Electromagnetic Actuation , 2000 .

[4]  James Lee,et al.  A Fault-Tolerant Magnetic Spin Stabilizing Controller for the JC2Sat-FF Mission , 2008 .

[5]  Marco Lovera,et al.  Periodic attitude control techniques for small satellites with magnetic actuators , 2002, IEEE Trans. Control. Syst. Technol..

[6]  Giulio Avanzini,et al.  Magnetic Detumbling of a Rigid Spacecraft , 2012 .

[7]  Mark L. Psiaki,et al.  Magnetic Torquer Attitude Control via Asymptotic Periodic Linear Quadratic Regulation , 2000 .

[8]  Gangbing Song,et al.  VIBRATION SUPPRESSION OF FLEXIBLE SPACECRAFT DURING ATTITUDE CONTROL , 2001 .

[9]  R. Bellman,et al.  The Riccati Equation , 1986 .

[10]  Christopher J. Damaren Hybrid magnetic attitude control gain selection , 2009 .

[12]  M. Pittelkau Optimal periodic control for spacecraft pointing and attitude determination , 1993 .

[13]  John Junkins,et al.  Optimal Estimation of Dynamic Systems, Second Edition , 2011 .

[14]  C. Damaren,et al.  Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control , 2011 .

[15]  Karthik Mysore Srinivasa SPACECRAFT ATTITUDE CONTROL USING MAGNETIC ACTUATORS , 2015 .

[16]  W. E. Boyce Elementary differential equations and boundary value problems / William E. Boyce, Richard C. DiPrima , 1996 .

[17]  Marco Lovera,et al.  Magnetic spacecraft attitude control: a survey and some new results , 2005 .

[18]  Keith A. Seffen,et al.  Folding and deployment of curved tape springs , 2000 .

[19]  Katsuhiko Ogata,et al.  Modern Control Engineering , 1970 .

[20]  Anton H. J. de Ruiter,et al.  A fault-tolerant magnetic spin stabilizing controller for the JC2Sat-FF mission , 2008 .

[21]  Christopher J. Damaren Comments on "Fully magnetic attitude control for spacecraft subject to gravity gradient" , 2002, Autom..

[22]  P. Hughes Spacecraft Attitude Dynamics , 1986 .

[23]  James R. Wertz,et al.  Spacecraft attitude determination and control , 1978 .

[24]  A. Astolfi,et al.  Global magnetic attitude control of spacecraft in the presence of gravity gradient , 2003, IEEE Transactions on Aerospace and Electronic Systems.

[25]  W. G. HUGHES Spacecraft Attitude Control , 1964, Nature.

[26]  Anton H. J. de Ruiter,et al.  Magnetic Control of Dual-Spin and Bias-Momentum Spacecraft , 2012 .

[27]  Rafael Wisniewski,et al.  Fully magnetic attitude control for spacecraft subject to gravity gradient , 1999, Autom..