Design of a Satellite Solar Panel Deployment Mechanism Using the Brushed DC Motor as Rotational Speed Damper
Authors: Hossein Ramezani Ali-Akbari
This paper presents an innovative method to control the rotational speed of a satellite solar panel during its deployment phase. A brushed DC motor has been utilized in the passive spring driven deployment mechanism to reduce the deployment speed. In order to use the DC motor as a damper, its connector terminals have been connected with an external resistance in a closed circuit. It means that, in this approach, there is no external power supply in the circuit. The working principle of this method is based on the back electromotive force (or back EMF) of the DC motor when an external torque (here the torque produced by the torsional springs) is coupled to the DC motor’s shaft. In fact, the DC motor converts to an electric generator and the current flows into the circuit and then produces the back EMF. Based on Lenz’s law, the generated current produced a torque which acts opposite to the applied external torque, and as a result, the deployment speed of the solar panel decreases. The main advantage of this method is to set an intended damping coefficient to the system via changing the external resistance. To produce the sufficient current, a gearbox has been assembled to the DC motor which magnifies the number of turns experienced by the DC motor. The coupled electro-mechanical equations of the system have been derived and solved, then, the obtained results have been presented. A full-scale prototype of the deployment mechanism has been built and tested. The potential application of brushed DC motors as a rotational speed damper has been successfully demonstrated.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1316259Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1083
 A. W. Bergquist, J. M. Jensen, B. J. Santiestevan, A. T. Vaughan, C. P. Vlastelica, C. D. Weaver, “Structures, mechanisms, launch vehicle selection,” Academic Course Report, Aerospace and Ocean Engineering Department, Virginia Tech, Blacksburg, VA. 2001.
 W. Shapiro, F. Murray, R. Howarth, and R. Fusaro, “Space mechanisms lessons learned study,” NASA TM-107046 and TM-107047., vols. I and II, 1995.
 M. C. Calassa, and R. Kackley, “Solar array deployment mechanism,” The 29th Aerospace Mechanisms Symposium, pp. 79-92. 1995.
 R. Stengel, “Spacecraft Mechanisms,” Lectures on Space System Design-Princeton University, MAE 342. 2008.
 G. Sneiderman, “Performance measurement of the sub-millimeter wave astronomy satellite (SWAS) solar array deployment system,” NASA, Goddard space flight center, Special payloads division, Greenbelt, Maryland 20771, 1995, Technical note.
 M. G. El-Sherbiny, A. Khattab, and M. K. Kassab, “Design of the deployment mechanism of solar array on a small satellite,” American Journal of Mechanical Engineering, vol. 1, No. 3, pp. 66-72. 2013.
 G. F. Abdelal, A. Bakr Elhady, and M. Kassab, “Design of a deployment rotation mechanism for micro-satellite,” International Journal for Simulation and Multidisciplinary Design Optimization, vol. 3, pp. 289-296. 2009.
 Q. Pan, T. He, D. Xiao, and X. Liu, “Design and damping analysis of a new eddy current damper for aerospace applications,” Latin American Journal of Solids and Structures, vpl. 13, No. 11, pp. 1997-2011. 2016.
 “Durango eddy current damper product catalog and design guidelines,” Avior Control Technologies, Inc., 2017. (www.AviorControls.com)
 H. A. Sodano, and J.-S. Bae, “Edyy current damping in structures,” Shock and Vibration Digest, vol. 36, No. 6, pp. 469-478. 2004.
 J.-S. Bae, M. K. Hwak, and D. J. Inman, “Vibration suppression of a cantilever beam using eddy current damper,” Journal of Sound and Vibration, vol. 284, Issues 3-5, pp. 805-824. 2005.
 L. Zaccarian, “DC motors: dynamic model and control techniques,” Teaching Material, homepages.laas.fr/lzaccari/seminars/DCmotors.pdf, Accessed on 18th November 2017.
 I. Vollmecke, “Parameter identification of DC motors,” Technical Report, www.imc-berlin.com, Accessed on 18th November 2017.
 F. Faulhaber, “DC-micromotors, Series 2232U,” Product Datasheet, www.faulhaber.com, Accessed on 18th November 2017.
 F. Faulhaber, “Planetary Gearheads, Series 22/7,” Product Datasheet, www.faulhaber.com, Accessed on 18th November 2017.