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No AccessEngineering Notes

Adaptive Momentum Distribution Jitter Control for Microsatellite

Published Online:https://doi.org/10.2514/1.G003909
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References

  • [1] Kahr E., Montenbruck O. and O'Keefe K. P. G., “Estimation and Analysis of Two-Line Elements for Small Satellites,” Journal of Spacecraft and Rockets, Vol. 50, No. 2, 2013, pp. 433–439. doi:https://doi.org/10.2514/1.A32352 JSCRAG 0022-4650 LinkGoogle Scholar

  • [2] Spangelo S. and Longmier B., “Optimization of CubeSat System-Level Design and Propulsion Systems for Earth-Escape Missions,” Journal of Spacecraft and Rockets, Vol. 52, No. 4, 2015, pp. 1009–1020. doi:https://doi.org/10.2514/1.A33136 JSCRAG 0022-4650 LinkGoogle Scholar

  • [3] Hudson J., Spangelo S., Hine A., Kolosa D. and Lemmer K., “Mission Analysis for CubeSats with Micro Propulsion,” Journal of Spacecraft and Rockets, Vol. 53, No. 5, 2016, pp. 836–846. doi:https://doi.org/10.2514/1.A33564 JSCRAG 0022-4650 LinkGoogle Scholar

  • [4] Watanabe H., Masuda K. and Uchiyama K., “Satellite Attitude Control System Using Three-Dimensional Reaction Wheel,” AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, AIAA Paper 2015-1782, 2015. doi:https://doi.org/10.2514/6.2015-1782 LinkGoogle Scholar

  • [5] Louke J. A., Schmidt E. S. and Young C. J., “An Open-Source Reaction Wheel System for Oregon’s First Satellite,” AIAA SPACE 2016, AIAA SPACE Forum, AIAA Paper 2016-5346, 2016. doi:https://doi.org/10.2514/6.2016-5346 LinkGoogle Scholar

  • [6] Katsukawa Y., Masada Y., Shimizu T., Sakai S. and Ichimoto K., “Pointing Stability of Hinode and Requirements for the Next Solar Mission Solar-C,” International Conference on Space Optics, Vol. 10565, SPIE, Bellingham WA, 2017, pp. 10565–10565–6. doi:https://doi.org/10.1117/12.2309171 Google Scholar

  • [7] Rizzo M. J., Rinehart S. A., Alcorn J. B., Barclay R. B., Barry R. K., Benford D. J., Dhabal A., Fixsen D. J., Gore A. S., Johnson-Shapoval S. and et al., “Building an Interferometer at the Edge of Space: Pointing and Phase Control System for BETTII,” Space Telescopes and Instrumentation 2014: Optical, Infrared, And Millimeter Wave, Vol. 9143, SPIE, Bellingham WA, 2014, Paper 91433H. doi:https://doi.org/10.1117/12.2055016 Google Scholar

  • [8] Remedia M., Aglietti G. S. and Richardson G., “A Stochastic Methodology for Predictions of the Environment Created by Multiple Micro Vibration Sources,” Journal of Sound and Vibration, Vol. 344, Feb. 2015, pp. 138–157. doi:https://doi.org/10.1016/j.jsv.2015.01.035 JSVIAG 0022-460X CrossrefGoogle Scholar

  • [9] Remedia M., Aglietti G. S., Richardson G. and Sweeting M., “Integrated Semi Empirical Methodology for Micro Vibration Prediction,” AIAA Journal, Vol. 53, No. 5, 2015, pp. 1236–1250. doi:https://doi.org/10.2514/1.J053339 AIAJAH 0001-1452 LinkGoogle Scholar

  • [10] Topland M. P. and Gravdah J. T., “Nonlinear Attitude Control of the Micro Satellite ESEO,” 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, International Astronautical Congress Paper  IAC-04-A.P.12, Vancouver, Canada, 2004. doi:https://doi.org/10.2514/6.IAC-04-A.P.12 AbstractGoogle Scholar

  • [11] Gross K., Hoffman J., Clark M., Swenson E., Cobb R., Whalen M. and Wagner L., “Evaluation of Formal Methods Tools Applied to a 6U CubeSat Attitude Control System,” AIAA SPACE 2015 Conference and Exposition, AIAA SPACE Forum, AIAA Paper 2015-4529, 2015. doi:https://doi.org/10.2514/6.2015-4529 LinkGoogle Scholar

  • [12] Gross K. H., Patrick R., Swenson E. and Agte J. S., “Optimal Attitude Control of a 6U CubeSat with a Four-Wheel Pyramid Reaction Wheel Array and Magnetic Torque Coils,” AIAA Modeling and Simulation Technologies Conference, AIAA SciTech Forum, AIAA Paper 2016-0174, 2016. doi:https://doi.org/10.2514/6.2016-0174 LinkGoogle Scholar

  • [13] Kjellberg H. C. and Lightsey E. G., “Discretized Constrained Attitude Pathfinding and Control for Satellites,” Journal of Guidance, Control, and Dynamics, Vol. 36, No. 5, 2013, pp. 1301–1309. doi:https://doi.org/10.2514/1.60189 JGCODS 0731-5090 LinkGoogle Scholar

  • [14] Zavoli A., De Matteis G., Giulietti F. and Avanzini G., “Single-Axis Pointing of an Underactuated Spacecraft Equipped with Two Reaction Wheels,” Journal of Guidance, Control, and Dynamics, Vol. 40, No. 6, 2017, pp. 1465–1471. doi:https://doi.org/10.2514/1.G002182 JGCODS 0731-5090 LinkGoogle Scholar

  • [15] Han Y., Biggs J. D. and Cui N., “Adaptive Fault-Tolerant Control of Spacecraft Attitude Dynamics with Actuator Failures,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 10, 2015, pp. 2033–2042. doi:https://doi.org/10.2514/1.G000921 JGCODS 0731-5090 LinkGoogle Scholar

  • [16] Inamori T., Wang J. H., Saisutjarit P. and Nakasuka S., “Jitter Reduction of a Reaction Wheel by Management of Angular Momentum Using Magnetic Torquers in Nano- and Micro-Satellites,” Advances in Space Research, Vol. 52, No. 1, 2013, pp. 222–231. doi:https://doi.org/10.1016/j.asr.2013.02.014 ASRSDW 0273-1177 CrossrefGoogle Scholar

  • [17] Bialke B., “High Fidelity Mathematical Modeling of Reaction Wheel Performance,” Advances in the Astronautical Sciences, Vol. 98, American Astronautical Soc. Paper 98-063, Springfield, VA, 1998, pp. 483–496. Google Scholar

  • [18] Masterson R. A., “Development and Validation of Empirical and Analytical Reaction Wheel Disturbance Models,” M.S. Thesis, Massachusetts Inst. of Technology, Cambridge, MA, 1999. Google Scholar

  • [19] Masterson R., Miller D. and Grogan R., “Development of Empirical and Analytical Reaction Wheel Disturbance Models,” 40th Structures, Structural Dynamics, and Materials Conference and Exhibit, Structures, Structural Dynamics, and Materials and Co-Located Conferences, AIAA Paper 1999-1204, 1999. doi:https://doi.org/10.2514/6.1999-1204. LinkGoogle Scholar

  • [20] Bialke B., “A Compilation of Reaction Wheel Induced Spacecraft Disturbances,” 20th Annual American Astronautical Society Guidance and Control Conference, American Astronautical Soc. Paper 97-038, Springfield, VA, 1997. Google Scholar

  • [21] Zhang Z., Aglietti G. S. and Zhou W. Y., “Microvibrations Induced by a Cantilevered Wheel Assembly with a Soft-Suspension System,” AIAA Journal, Vol. 49, No. 5, 2011, pp. 1067–1079. doi:https://doi.org/10.2514/1.J050791 AIAJAH 0001-1452 LinkGoogle Scholar

  • [22] Zhang Z., Aglietti G. S. and Ren W. J., “Coupled Microvibration Analysis of a Reaction Wheel Assembly Including Gyroscopic Effects in its Accelerance,” Journal of Sound and Vibration, Vol. 332, No. 22, 2013, pp. 5748–5765. doi:https://doi.org/10.1016/j.jsv.2013.06.011 JSVIAG 0022-460X CrossrefGoogle Scholar

  • [23] Addari D., Aglietti G. S. and Remedia M., “Experimental and Numerical Investigation of Coupled Microvibration Dynamics for Satellite Reaction Wheels,” Journal of Sound and Vibration, Vol. 386, Oct. 2017, pp. 225–241. doi:https://doi.org/10.1016/j.jsv.2016.10.003 JSVIAG 0022-460X CrossrefGoogle Scholar

  • [24] Addari D., Aglietti G. S. and Remedia M., “Dynamic Mass of a Reaction Wheel Including Gyroscopic Effects: An Experimental Approach,” AIAA Journal, Vol. 55, No. 1, 2017, pp. 274–285. doi:https://doi.org/10.2514/1.J055398 AIAJAH 0001-1452 LinkGoogle Scholar

  • [25] Peng C., Fang J. C. and Cui P. L., “Dynamics Modeling and Measurement of the Microvibrations for a Magnetically Suspended Flywheel,” IEEE Transactions on Instrumentation and Measurement, Vol. 64, No. 12, 2015, pp. 3239–3252. doi:https://doi.org/10.1109/TIM.2015.2459491 IEIMAO 0018-9456 CrossrefGoogle Scholar

  • [26] Wang H., Han Q. K., Luo R. Z. and Qing T., “Dynamic Modeling of Moment Wheel Assemblies with Nonlinear Rolling Bearing Supports,” Journal of Sound and Vibration, Vol. 406, June 2017, pp. 124–145. doi:https://doi.org/10.1016/j.jsv.2017.06.019 JSVIAG 0022-460X CrossrefGoogle Scholar

  • [27] Alcorn J., Allard C. J. and Schaub H., “Fully-Coupled Dynamical Jitter Modeling of a Rigid Spacecraft with Imbalanced Reaction Wheels,” AIAA/AAS Astrodynamics Specialist Conference, AIAA SPACE Forum, AIAA Paper 2016-5686, 2016. doi:https://doi.org/10.2514/6.2016-5686 LinkGoogle Scholar

  • [28] Markley F. L. and Crassidis J. L., Fundamentals of Spacecraft Attitude Determination and Control, Springer–Verlag, New York, 2014, p. 345–359. CrossrefGoogle Scholar

  • [29] Wie B. and Barba P., “Quaternion Feedback for Spacecraft Large Angle Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 360–365. doi:https://doi.org/10.2514/3.19988 JGCODS 0731-5090 LinkGoogle Scholar

  • [30] Wie B., Weiss H. and Arapostathis A., “A Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations,” Guidance, Navigation and Control Conference, AIAA Paper 1988-4128, 1988. doi:https://doi.org/10.2514/6.1988-4128 LinkGoogle Scholar

  • [31] Bošković J. D., Li S. M. and Mehra R. K., “Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation,” Journal of Guidance, Control, and Dynamics, Vol. 24, No. 1, 2001, pp. 14–22. doi:https://doi.org/10.2514/2.4704 JGCODS 0731-5090 LinkGoogle Scholar