علوم و فناوری فضایی

علوم و فناوری فضایی

مروری بر کنترل وضعیت زیرتحریک ماهواره های تحریک شده با چرخ عکس العملی

نوع مقاله : مقالة‌ مروری‌

نویسندگان
1 دکتری، دانشکده مهندسی هوافضا، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران، ایران.
2 دانشیار، دانشکده مهندسی هوافضا، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران، ایران.
3 استادیار، دانشکده مهندسی هوافضا، دانشگاه صنعتی خواجه نصیرالدین طوسی، تهران، ایران
چکیده
زیرسیستم تعیین و کنترل وضعیت یکی از زیرسیستم های حیاتی ماهواره است که امکان انجام مانور و نشانه روی را فراهم می کند. طبق آمار، بیش از نیمی از ماهواره های کوچک پرتاب شده، از چرخ عکس العملی به عنوان عملگر روی برد برای تکمیل وظیفه ی مانور وضعیت استفاده می کنند. اصطلاح فنی زیرتحریک برای توصیف سیستم هایی که تعداد عملگر کمتری نسبت به درجات آزادی خود دارند، استفاده می شود. محدودیت های ساختاری و خرابی عملگر، می توانند منجر به یک سیستم زیرتحریک شوند. زیرتحریک شدن ماهواره در یک شرایط عملیاتی می تواند عملکرد روی مدار آن را کاهش داده و باعث شکست در مأموریت شود. در این مقاله ابتدا ماهواره ی زیرتحریک معرفی شده و مروری بر روش های کنترل وضعیت ماهواره در شرایط سالم شده است. در ادامه کنترل تحمل پذیر عیب و انواع مکانیزم های شناسایی شرایط زیرتحریک ارائه می شوند. ﺍﺳﺘﻔﺎﺩﻩ ﺍﺯ ﺭﻭﺵﻫﺎﻱ ﻣﺒﺘﻨﻲ ﺑﺮ ﻣـﺪﻝ به دلیل تناسب با تکنیک های کنترلی جبران سازی عیب و کارآیی در تمامی شرایط عملیاتی ماهواره، جهت تشخیص شرایط زیرتحریک مناسب است. همچنین عمده کارهای ﺻﻮﺭﺕ ﮔﺮﻓﺘﻪ ﻣﺘﻤﺮﮐﺰ ﺑﺮ مشاهده گر ﺍﺳﺖ. همچنین روش هایی که به منظور پایداری و کنترل یک ماهواره زیرتحریک با استفاده از عملگر چرخ عکس العملی به کار رفته اند، بررسی می شود. در انتها نیز کنترل تعقیب وضعیت در شرایط زیرتحریک آمده است.
کلیدواژه‌ها
موضوعات

[1]   S. S. Nudehi, U. Farooq, A. Alasty, and J. Issa, "Satellite attitude control using three reaction wheels," in American Control Conference, Seattle, WA, USA, 2008, pp. 4850-4855, https://doi.org/10.1109/ACC.2008.4587262.
[2]   M. Rivandi, M. Mirshams, and M. Zarourati, "Design and implementation of a balance system for the cubesat attitude determination and control tabletop simulator," Journal of Space Science and Technology, vol. 16, no. 1, pp. 75–88, 2023, (in Persian), https://doi.org/10.30699/jsst.2023.1426.
[3]   L. Briguglio, Handbook of Small States: Economic, Social and Environmental Issues, 1st ed. London: Routledge, 2018, https://doi.org/10.4324/9781351181846.
[4]   T. Urakubo, K. Tsuchiya, and K. Tsujita, "Attitude control of a spacecraft with two reaction wheels," Journal of Vibration and Control, vol. 10, no. 9, pp. 1291–311, 2004, https://doi.org/10.1177/1077546304042042.
[5]   M. Flynn, F. Leve, C. Petersen, and I. Kolmanovsky, "Linear control of underactuated spacecraft with two reaction wheels made feasible by solar radiation pressure," in American Control Conference (ACC), Chicago, IL, USA, 2015, pp. 3193-3198, https://doi.org/10.1109/ACC.2015.7171824.
[6]   N. M. Horri and S. Hodgart, "Attitude stabilization of an underactuated satellite using two wheels," in Aerospace Conference Proceedings (Cat. No.03TH8652), Big Sky, MT, USA, 2003, pp. 6_2629-6_2635, https://doi.org/10.1109/AERO.2003.1235188.
[7]   B. He, S. Wang, and Y. Liu, "Underactuated robotics: A review," International Journal of Advanced Robotic Systems, vol. 16, no. 4, 2019, https://doi.org/10.1177/1729881419862164.
[8]   M. Zarourati, M. Mirshams, and M. Tayefi, "Designing an adaptive robust observer for underactuation fault diagnosis of a remote sensing satellite," International Journal of Adaptive Control and Signal Processing, vol. 37, no. 11, pp. 2812-2834, 2023, https://doi.org/10.1002/acs.3661.
[9]   H. W. Moos et al., "Overview of the Far Ultraviolet Spectroscopic Explorer Mission," the Astrophysical Journal, vol. 538, no. 1, 2000, Art. no. L1–6, https://doi.org/10.1086/312795.
[10] R. Cowen, "The wheels come off Kepler," Nature Publishing Group, vol. 497, no. 7450, 2013.
[11] J. Eickhoff, Onboard computers, onboard software and satellite operations: An introduction, Berlin, Heidelberg: Springer, 2012, https://doi.org/10.1007/978-3-642-25170-2.
[12] Q. M. Lam and I. Barkana, "A close examination of under-actuated attitude control subsystem design for future satellite missions’ life extension," in 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, vol. 1637, no. 1, Narvik, Norway, 2014, pp. 555–564, https://doi.org/10.1063/1.4904624.
[13]F. L. Markley and J. L. Crassidis, Fundamentals of Spacecraft Attitude Determination and Control, New York: Springer, 2014, https://doi.org/10.1007/978-1-4939-0802-8.
[14]I. Gueddi, O. Nasri, and K. Ben Othman, "A new interval diagnosis method: Application to the spacecraft rendezvous phase of the Mars sample return mission," International Journal of Adaptive Control and Signal Processing, vol. 34, no. 1, pp. 42-62, 2019, https://doi.org/10.1002/acs.3065.
[15] M. Zarourati, M. Mirshams, and M. Tayefi, "Active underactuation fault-tolerant backstepping attitude tracking control of a satellite with interval error constraints," Advanced Control for Applications, vol. 6, no. 3, 2024, Art. no. e215, https://doi.org/10.1002/adc2.215.
[16] R. Isermann and P. Ballé, "Trends in the application of model-based fault detection and diagnosis of technical processes," Control Engineering Practice, vol. 5, no. 5, pp. 709-719, 1997, https://doi.org/10.1016/S0967-0661(97)00053-1.
[17] B. Geometric, "Goodwine control of mechanical systems: Book review," IEEE Transactions on Automatic Control, vol. 50, no. 12, Paper 2111, 2005, https://doi.org/10.1109/TAC.2005.860277.
[18] R. Isermann, Fault-Diagnosis Applications, Model-Based Condition Monitoring: Actuators, Drives, Machinery, Plants, Sensors, and Fault-tolerant Systems, Springer Berlin, Heidelberg, 2011, https://doi.org/10.1007/978-3-642-12767-0.
[19] R. N. Banavar and V. Sankaranarayanan, Switched Finite Time Control of a Class of Underactuated Systems, Springer Berlin, Heidelberg, 2006, https://doi.org/10.1007/11616269.
[20] C. D. Petersen, F. Leve, and I. Kolmanovsky, "Model predictive control of an underactuated spacecraft with two reaction wheels," Journal of Guidance, Control, and Dynamics, vol. 40, no. 2, pp. 320-332, 2017, https://doi.org/10.2514/1.G000320.
[21] C. D. Petersen, F. Leve, and I. Kolmanovsky, "Underactuated spacecraft switching law for two reaction wheels and constant angular momentum,' Journal of Guidance, Control, and Dynamics, vol. 39, no. 9, pp. 2086–2099, 2016, https://doi.org/10.2514/1.G001680.
[22] H. Gui, L. Jin, and S. Xu, "Attitude maneuver control of a two-wheeled spacecraft with bounded wheel speeds," Acta Astronautica, vol. 88, pp. 98-107, 2013, https://doi.org/10.1016/j.actaastro.2013.03.006.
[23] H. J. Kramer, Observation of the Earth and Its Environment, Survey of Missions and Sensors, 4th ed. Springer Berlin, Heidelberg, 2002, https://doi.org/10.1007/978-3-642-56294-5.
[24] J. F. Castet and J. H. Saleh, "Satellite and satellite subsystems reliability: Statistical data analysis and modeling," Reliability Engineering & System Safety, vol. 94, no. 11, pp. 1718-1728, 2009,  https://doi.org/10.1016/j.ress.2009.05.004.
[25] E. Sobhani-Tehrani and K. Khorasani, Fault Diagnosis of Nonlinear Systems Using a Hybrid Approach, Springer New York, NY; 2009, https://doi.org/10.1007/978-0-387-92907-1.
[26] H. B. Hassrizal and J. A. Rossiter, "A survey of control strategies for spacecraft attitude and orientation," in 11th International Conference on Control (CONTROL), Belfast, UK, 2016, pp. 1-6, https://doi.org/10.1109/CONTROL.2016.7737543.
[27] M. Tafazoli, "A study of on-orbit spacecraft failures," Acta Astronautica, vol. 64, no. 2-3, pp. 195–205, 2009, https://doi.org/10.1016/j.actaastro.2008.07.019.
[28] J. K. Wayer, J. F. Castet, and J. F. Saleh, "Spacecraft attitude control subsystem: Reliability, multi-state analyses, and comparative failure behavior in LEO and GEO," Acta Astronautica, vol. 85, pp. 83–92, 2013, https://doi.org/10.1016/j.actaastro.2012.12.003.
[29] Q. Hu, B. Xiao, B. Li, and Y. Zhang, Fault-Tolerant Attitude Control of Spacecraft, Elsevier, 2021, https://doi.org/10.1016/c2020-0-03287-1.
[30] L. He, W. Ma, P. Guo, and T. Sheng, "Developments of attitude determination and control system of microsats: A survey," Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, vol. 235, no. 10, pp. 1733–1750, 2020,  https://doi.org/10.1177/0959651819895173.
[31] R. Isermann, Fault-Diagnosis Systems: An Introduction from Fault Detection to Fault Tolerance, Springer Berlin, Heidelberg, 2006, https://doi.org/10.1007/3-540-30368-5.
[32] A. M. Cruise, J. A. Bowles, T. J. Patrick, and C. V. Goodall, Principles of Space Instrument Design, Cambridge University Press, 1998, https://doi.org/10.1017/CBO9780511584503.
[33] N. Tudoroiu and K. Khorasani, "Satellite fault diagnosis using a bank of interacting Kalman filters," IEEE Transactions on Aerospace and Electronic Systems, vol. 43, no. 4, pp. 1334–1350, 2007,  https://doi.org/10.1109/TAES.2007.4441743.
[34] Y. Bai, J. D. Biggs, X. Wang, and N. Cui, "Attitude tracking with an adaptive sliding mode response to reaction wheel failure," European Journal of Control, vol. 42, pp. 67–76, 2018, https://doi.org/10.1016/j.ejcon.2018.02.008.
[35]R. Qi, W. Su, and Y. Meng, "Fault-tolerant attitude controller design for deep space probe via adaptive fast terminal sliding mode control," Journal of Dynamic Systems, Measurement, and Control, vol. 141, no. 9, 2019, Art. no. 091006, https://doi.org/10.1115/1.4042548.
[36] Q. Shen, C. Yue, C. H. Goh, and D. Wang, "Active fault-tolerant control system design for spacecraft attitude maneuvers with actuator saturation and faults," IEEE Transactions on Industrial Electronics, vol. 66, no. 5, pp. 3763-3772, 2019, https://doi.org/ 10.1109/TIE.2018.2854602.
[37]Z. Ismail, R. Varatharajoo, and Y. C.Chak, "A fractional-order sliding mode control for nominal and underactuated satellite attitude controls," Advances in Space Research, vol. 66, no. 2, pp. 321–334, 2020, https://doi.org/10.1016/j.asr.2020.02.022.
[38]A. Fan, H. Huang, and K. Zhou, "Robust fault-tolerant attitude control for satellite with multiple uncertainties and actuator faults," Chinese Journal of Aeronautics, vol. 33, no. 12, pp. 3380–3394, 2020,  https://doi.org/10.1016/j.cja.2020.06.026.
[39] Z. Yuan, L. Wu, and X. Yao, "Adaptive fault-tolerant attitude-tracking control of spacecraft with quantized control torque," IEEE Access, vol. 8, pp. 226653–226661, 2020, https://doi.org/10.1109/ACCESS.2020.3045017.
[40] D. Lee and H. Leeghim, "Reaction wheel fault-tolerant finite-time control for spacecraft attitude tracking without unwinding," International Journal of Robust and Nonlinear Control, vol. 30, no. 9, pp. 3672–3691, 2020, https://doi.org/10.1002/rnc.4957.
[41] X. Shao, Q. Hu, Y. Shi, and Y. Zhang, "Fault-tolerant control for full-state error constrained attitude tracking of uncertain spacecraft," Automatica, vol. 151, 2023, Art. no. 110907, https://doi.org/10.1016/j.automatica.2023.110907.
[42] Q. Huang and Y. Zhang, "Continuous appointed-time prescribed performance attitude tracking control for rigid spacecraft with actuator faults on SO(3)," International Journal of Robust and Nonlinear Control, vol. 34, no. 1, pp. 628-647, 2023, https://doi.org/10.1002/rnc.6991.
[43] J. D. Biggs, Y. Bai, and H. Henninger, "Attitude guidance and tracking for spacecraft with two reaction wheels," International Journal of Control, vol. 91, no. 4, pp. 926–936, 2017, https://doi.org/10.1080/00207179.2017.1299944
[44] M. Zarourati, M. Mirshams, and M. Tayefi, "Adaptive robust attitude control and vibration suppression of a flexible satellite in imaging maneuver," Journal of Space Science and Technology, vol. 18, no. 1, pp. 78–91, 2025, (in Persian), https://doi.org/10.22034/jsst.2025.1524.
[45] P. Gasbarri, R. Monti, and M. Sabatini, "Very large space structures: Non-linear control and robustness to structural uncertainties," Acta Astronautica, vol. 93, pp. 252–265, 2014, https://doi.org/10.1016/j.actaastro.2013.07.022.
[46] L. Cao. X. Chen, and B. Xiao, Predictive Filtering for Microsatellite Control System, Elsevier, 2020, https://doi.org/10.1016/C2019-0-04217-3.
[47] Y. Yang, "Analytic LQR design for spacecraft control system based on quaternion model," Journal of Aerospace Engineering, vol. 25, no. 3, pp. 448–453, 2012, https://doi.org/10.1061/(ASCE)AS.1943-5525.000014.
[48] M. Navabi and M. R. Hosseini, "Spacecraft quaternion based attitude input-output feedback linearization control using reaction wheels," in 8th International Conference on Recent Advances in Space Technologies (RAST), Istanbul, Turkey, 2017, pp. 97–103, https://doi.org/10.1109/RAST.2017.8002994.
[49] Y. Li, Z. Sun, and  D. Ye, "Robust linear PID controller for satellite attitude stabilisation and attitude tracking control," International Journal of Space Science and Engineering, vol. 4, no. 1, pp. 64-75, 2016, https://doi.org/10.1504/IJSPACESE.2016.078581.
[50] S. Shen and Q. Sun, "Characteristic model-based fast attitude maneuver for the complex flexible satellite," AIAA SPACE 2015 Conference and Exposition, Pasadena, California, 2015, https://doi.org/10.2514/6.2015-4508.
[51] G. P. Yuan, X. P. Shi, and L. Li, "Adaptive robust attitude controler design for spacecraft," Systems Engineering and Electronic Technology, vol. 34, no. 12, pp. 2524-2528, 2012, https://doi.org/10.3969/j.issn.1001-506X.2012.12.21.
[52] L. Wang, Y. Guo, W. Yao, and Q. Chen, "Adaptive robust attitude control for flexible spacecraft with control moment gyroscopes," in 12th World Congress on Intelligent Control and Automation (WCICA), Guilin, China, 2016, pp. 2376–2381, https://doi.org/10.1109/WCICA.2016.7578603.
[53] M. Zarourati, M. Mirshams, and M Tayefi, "Attitude path design and adaptive robust tracking control of a remote sensing satellite in various imaging modes," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 237, no. 9, pp. 2166–2184, 2023, https://doi.org/10.1177/09544100221148887.
[54] F. L. Markley, R. G. Reynolds, F. X. Liu, ana K. L. Lebsock, "Maximum torque and momentum envelopes for reaction-wheel arrays," Journal of Guidance, Control, and Dynamics, vol. 33, no. 5, pp. 1606–1614, 2012, https://doi.org/10.2514/1.47235.
[55] H. Gui, G. Vukovich, and S. Xu, "Attitude tracking of a rigid spacecraft using two internal torques," IEEE Transactions on Aerospace and Electronic Systems, vol. 1, no. 4, pp. 2900–2913, 2015, https://doi.org/ 10.1109/TAES.2015.140670.
[56] C. Yue, K. D. Kumar, Q. Shen, C. H. Goh, and T. H. Lee, "Attitude stabilization using two parallel single-gimbal control moment gyroscopes," Journal of  Guidance, Control, and Dynamics, vol. 42, no. 6, pp. 1353–1364, 2019, https://doi.org/10.2514/1.G003445.
[57] J. H. Lee, D. Kim, J. Kim, and H. S. Oh, "Shorter path design and control for an underactuated satellite," International Journal of Aerospace Engineering, vol. 2017, no. 1, 2017, Art. no. 8536732 https://doi.org/10.1155/2017/8536732.
[58] Z. Ismail and R. Varatharajoo, "A study of reaction wheel configurations for a 3-axis satellite attitude control," Advances in Space Research, vol. 45, no. 6, pp. 750–759, 2010, https://doi.org/10.1016/j.asr.2009.11.004.
[59] J. Qiao, D. Zhang, Y. Zhu, and P. Zhang, "Disturbance observer-based finite-time attitude maneuver control for micro satellite under actuator deviation fault," Aerospace Science and Technology, vol. 82-83, pp. 262-271, 2018, https://doi.org/10.1016/j.ast.2018.09.007.
[60] Y. Wu, G. Zhang, L. Wu, and W. Hu, "Observer-based finite time adaptive fault tolerant control for nonaffine nonlinear systems with actuator faults and disturbances," International Journal of Adaptive Control and Signal Processing, vol. 34, no. 10, pp. 1430-144634, 2020, https://doi.org/10.1002/acs.3158.
[61] P. Castaldi, N. Mimmo, and S. Simani, "LEO satellite active FTC with aerodynamic disturbance decoupled fault diagnosis," European Journal of Control, vol. 51, pp. 76-94, 2020, https://doi.org/10.1016/j.ejcon.2019.06.005.
[62] H. Lee and Y. Kim, "Fault-tolerant control scheme for satellite attitude control system," IET Control Theory & Applications, vol. 4, no. 8, pp. 1436-1450, 2010, https://doi.org/10.1049/iet-cta.2009.0159.
[63] Z. Q. Li, L. Ma, and K. Khorasani, "A dynamic neural network-based reaction wheel fault diagnosis for satellites," in International Joint Conference on Neural Network Proceedings, Vancouver, BC, Canada, 2006, pp. 3714–3721, https://doi.org/10.1109/IJCNN.2006.247387.
[64] Y. Wei, L. Sheng, J. Fang, and M. Gao, "Adaptive fault-tolerant tracking control for nonlinear systems with unknown control coefficient and input saturation," International Journal of Adaptive Control and Signal Processing, vol. 37, no. 2, pp. 414-435, 2022, https://doi.org/10.1002/acs.3547.
[65]Z. Kang, Q. Shen, S. Wu, and C. J. Damaren, "Saturated attitude control of multispacecraft systems on SO(3) subject to mixed attitude constraints with arbitrary initial attitude," IEEE Transactions on Aerospace and Electronic, vol. 59, no. 5, pp. 5158-5173, 2023, https://doi.org/10.1109/TAES.2023.3251972.
[66] X. Yue, J. Liu, K. Chen, Y. Zhang, and Z. Hu, "Prescribed performance adaptive event-triggered consensus control for multiagent systems with input saturation," Frontiers in Neurorobotics, vol. 16, 2023, https://doi.org/10.3389/fnbot.2022.1103462.
[67] C. Han, J. Guo, and A. Pechev, "Nonlinear H based underactuated attitude control for small satellites with two reaction wheels," Acta Astronautica, vol. 104, no. 1, pp. 159–172, 2014, https://doi.org/10.1016/j.actaastro.2014.07.036.
[68] J. Gertler, Fault Detection and Diagnosis in Engineering Systems, 1st ed. Boca Raton: CRC Press, 2017, https://doi.org/10.1201/9780203756126.
[69] R. Isermann, "Supervision, fault-detection and fault-diagnosis methods– a short introduction," in Combust. Engine Diagnosis, Model-Based Condition Monitoring of Gasoline and Diesel Engines and Their Components, Berlin, Heidelberg: Springer, 2017, pp. 25–47, https://doi.org/10.1007/978-3-662-49467-7_2.
[70] Y. Zhang and J. Jiang, "Bibliographical review on reconfigurable fault-tolerant control systems," Annual Reviews in Control, vol. 32, no. 2, pp. 229-252, 2008, https://doi.org/10.1016/j.arcontrol.2008.03.008.
[71] S. Yin, B. Xiao, S. X. Ding, and D. Zhou, "A review on recent development of spacecraft attitude fault tolerant control system," IEEE Transactions on Industrial Electronics, vol. 63, no. 5, pp. 3311–3320, 2016, https://doi.org/ 10.1109/TIE.2016.2530789.
[72] S. Gao, W. Zhang, and X. He, "Observer-based multiple faults diagnosis scheme for satellite attitude control system," Asian Journal of Control, vol. 22, no. 1, pp. 307-322, 2018, https://doi.org/10.1002/asjc.1873.
[73] H. Alwi, C. Edwards, and C. Pin Tan, Fault Detection and Fault-Tolerant Control Using Sliding Modes, London: Springer, 2011, https://doi.org/10.1007/978-0-85729-650-4.
[74] S. Simani, C. Fantuzzi, and R. J. Patton, Model-based Fault Diagnosis in Dynamic Systems Using Identification Techniques, London: Springer, 2003, https://doi.org/10.1007/978-1-4471-3829-7.
[75] B. Xiao, Q. Hu, Y. Zhang, and X. Huo, "Fault-tolerant tracking control of spacecraft with attitude-only measurement under actuator failures," Journal of Guidance, Control, and Dynamics, vol. 37, no. 3, pp. 838–849, 2014, https://doi.org/10.2514/1.61369.
[76] X. Zhang and Z. Zhou, "Integrated fault estimation and fault tolerant attitude control for rigid spacecraft with multiple actuator faults and saturation," IET Control Theory & Applications, vol. 13, no. 15, pp. 2365-2375, 2019, https://doi.org/10.1049/iet-cta.2019.0195.
[77] Q. Hu, X. Zhang, and G. Niu, "Observer-based fault tolerant control and experimental verification for rigid spacecraft," Aerospace Science and Technology, vol. 92, pp. 373-386, https://doi.org/10.1016/j.ast.2019.06.013.
[78] I. Hwang, S. Kim, Y. Kim, and C. E. Seah, "A survey of fault detection, isolation, and reconfiguration methods," IEEE Transactions on Control Systems Technology, vol. 18, no. 3, pp. 636-653, 2010, https://doi.org/10.1109/TCST.2009.2026285.
[79] H. Henna, H. Toubakh, M. R. Kafi, and M. S. Mouchaweh, "Towards fault-tolerant strategy in satellite attitude control systems: A review," in 12th Annual Conference of the Prognostics and Health Management Society, vol. 12, no. 1, virtual conference, 2020, https://doi.org/10.36001/phmconf.2020.v12i1.1272.
[80] C. Gao, Q. Zhao, and G. Duan, "Robust actuator fault diagnosis scheme for satellite attitude control systems," Journal of the Franklin Institute, vol. 350, no. 9, pp. 2560-2580, 2013, https://doi.org/10.1016/j.jfranklin.2013.02.021.
[81] Z. Gao, Z. Zhou, G. Jiang, M. Qian, and J. Lin, "Active fault tolerant control scheme for satellite attitude systems: Multiple actuator faults case," International Journal of Control, Automation and Systems, vol. 16, pp. 1794–1804, 2018, https://doi.org/10.1007/s12555-016-0667-5.
[82] D. Henry, "Fault diagnosis of microscope satellite thrusters using H-infinity/H_ filters," Journal of Guidance, Control, and Dynamics, vol. 31, no. 3, pp. 699–711, 2008, https://doi.org/10.2514/1.31003.
[83] P. Baldi, M. Blanke, P. Castaldi, N. Mimmo, and S. Simani, "Fault diagnosis for satellite sensors and actuators using nonlinear geometric approach and adaptive observers," International Journal of Robust and Nonlinear Control, vol. 29, no. 16, pp. 5429-5455, 2018, https://doi.org/10.1002/rnc.4083.
[84]S. Zhu, D. Wang, Q. Shen, and E. K. Poh, "Satellite attitude stabilization control with actuator faults," Journal of Guidance, Control, and Dynamics, vol. 40, no. 5, pp. 1300–1309, 2017, https://doi.org/10.2514/1.G001922.
[85] Z. Gao, Z. Zhou, M. S. Qian, and J. Lin, "Active fault tolerant control scheme for satellite attitude system subject to actuator time-varying faults," IET Control Theory & Applications, vol. 12, no. 3, pp. 405-412, 2018, https://doi.org/10.1049/iet-cta.2017.0969.
[86] Z. Gao, B. Jiang, P. Shi, M. Qian, and J. Lin, "Active fault tolerant control design for reusable launch vehicle using adaptive sliding mode technique," Journal of the Franklin Institute, vol. 349, no. 4, pp. 1543–1560, 2012, https://doi.org/10.1016/j.jfranklin.2011.11.003.
[87] H. Li, Q. Jia, R. Ma, and X. Chen, "Observer-based robust actuator fault isolation and identification for microsatellite attitude control systems," Aircraft Engineering and Aerospace Technology, vol. 93, no. 7, pp. 1145–1155, 2021, https://doi.org/10.1108/AEAT-10-2020-0224.
[88] G. Chen and Y. D. Song, "Robust fault-tolerant cooperative control of multi-agent systems: A constructive design method," Journal of the Franklin Institute, vol. 352, no. 10, pp. 4045-4066, 2015, https://doi.org/10.1016/j.jfranklin.2015.05.031.
[89] F. Nemati, S. M. Safavi Hamami, and A. Zemouche, "A nonlinear observer-based approach to fault detection, isolation and estimation for satellite formation flight application," Automatica, vol. 107, pp. 474–482, 2019, https://doi.org/10.1016/j.automatica.2019.06.007.
[90] L. de. p. Carvalho, F. Y. Toriumi, B. A. Angélico, and O. L. do. V. Costa, "Model-based fault detection filter for Markovian jump linear systems applied to a control moment gyroscope," European Journal of Control, vol. 59, pp. 99-108, 2021, https://doi.org/10.1016/j.ejcon.2021.02.003.
[91] X. L. Yao, G. Tao, B. Jiang, and X. H. Lv, "Stabilization of an underactuated rigid body with unknown parameters using adaptive switching control," in Chinese Guidance, Navigation and Control Conference, Yantai, China, 2014, pp. 1573–1578, https://doi.org/10.1109/CGNCC.2014.7007427.
[92] Q. Hu, B. Li, B. Xiao, and Y. Zhang, Control Allocation for Spacecraft Under Actuator Faults, Springer Singapore, 2021, https://doi.org/10.1007/978-981-16-0439-3.
[93] H. Hermes, "On a stabilizing feedback attitude control," Journal of Optimization Theory and Applications, vol. 31, pp. 373–384, 1980, https://doi.org/10.1007/BF01262979.
[94] P. C. Crouch, "Spacecraft attitude control and stabilization: applications of geometric control theory to rigid body models," IEEE Transactions on Automatic Control, vol. 29, no. 4, pp. 321–331, 1984, https://doi.org/10.1109/TAC.1984.1103519.
[95] H. Yadegari, H. Chao, and Z. Yukai, "Finite time sliding mode controller for a rigid satellite in presence of actuator failure," in 3rd International Conference on Information Science and Control Engineering (ICISCE), Beijing, China, 2016, pp. 1327–1331, https://doi.org/10.1109/ICISCE.2016.283.
[96] B. Li, Q. Hu, Y. Yang, and O. A. Postolache, "Finite-time disturbance observer based integral sliding mode control for attitude stabilisation under actuator failure," IET Control Theory & Applications, vol. 13, no. 1, pp. 50-58, 2019, https://doi.org/10.1049/iet-cta.2018.5477.
[97] E. D. Sontag and H. J. Sussmann, "Further comments on the stabilizability of the angular velocity of a rigid body," Systems & Control Letters, vol. 12, no. 3, pp. 213-217, 1989, https://doi.org/10.1016/0167-6911(89)90052-2.
[98] P. Morin, "Robust stabilisation of the angular velocity of a rigid body with two controls," European Journal of Control, vol. 2, no. 1, pp. 51-56, 1996, https://doi.org/10.1016/S0947-3580(96)70028-6.
[99] V. Coverstone-Carroll, "Detumbling and reorienting underactuated rigid spacecraft," Journal of Guidance, Control, and Dynamics, vol. 19, no. 3, pp. 708–710, 1996, https://doi.org/10.2514/3.21680.
[100]D. Aeyels, "Stabilization by smooth feedback of the angular velocity of a rigid body," Systems & Control Letters, vol. 6, no. 1, pp. 59-63, 1985, https://doi.org/10.1016/0167-6911(85)90055-6.
[101]C. I. Byrnes and A. Isidori, "On the attitude stabilization of rigid spacecraft," Automatica, vol. 27, no. 1, pp. 87-95, 1991, https://doi.org/10.1016/0005-1098(91)90008-P.
[102]C. I. Byrnes, S. Monaco, A. Isidori, and S. Sabatino, "Analysis and simulation of a controlled rigid spacecraft: Stability and instability near attractors," in 27th Conference on Decision and Control, Austin, TX, USA, 1988, pp. 81–85, https://doi.org/10.1109/CDC.1988.194273.
[103]H. Krishnan, N. H. McClamroch, and M. Reyhanoglu, "Attitude stabilization of a rigid spacecraft using two momentum wheel actuators," Journal of Guidance, Control, and Dynamics, vol. 18, no. 2, pp. 256–263, 1995, https://doi.org/10.2514/3.21378.
[104]E. Y, Kerai, "Analysis of small time local controllability of the rigid body model," IFAC Proceedings Volumes, vol. 28, no. 8, pp. 597-602, 1995, https://doi.org/10.1016/S1474-6670(17)45529-7.
[105]F. Boyer and M. Alamir, "Further results on the controllability of a two-wheeled satellite," Journal of Guidance, Control, and Dynamics, vol. 30, no. 2, pp. 611–619, 2007, https://doi.org/10.2514/1.21505.
[106]. Kim and Y. Kim, "Spin-axis stabilization of a rigid spacecraft using two reaction wheels," Journal of Guidance, Control, and Dynamics, vol. 24, no. 5, pp. 1046–1049, 2001, https://doi.org/10.2514/2.4818.
[107]y. Katsuyama, K. Sekiguchi, and M. Sampei, "Spacecraft attitude control by 2 wheels with initial angular momentum," in SICE Annual Conference, Nagoya, Japan, 2013, pp. 1890-1895.
[108]L. Jin and S. Xu, "Underactuated spacecraft angular velocity stabilization and three-axis attitude stabilization using two single gimbal control moment gyros," Acta Mechanica Sinica, vol. 26, pp. 279-288, 2010, https://doi.org/10.1007/s10409-009-0272-4.
[109]S. Kwon, T. Shimomura, and H. Okubo, "Pointing control of spacecraft using two SGCMGs via LPV control theory," Acta Astronautica, vol. 68, no. 7-8, pp. 1168-1175, 2011, https://doi.org/10.1016/j.actaastro.2010.10.001.
[110]R. W. Brockett, "Asymptotic stability and feedback stabilization," Differential geometric control theory, vol. 27, no. 1, pp. 181-191, 1983.
[111]J. Zabczyk, "Some comments on stabilizability," Applied Mathematics and Optimization, vol. 19, pp. 1-9, 1989, https://doi.org/10.1007/BF01448189.
[112]L. Gurvits and Z. X. Li, "Smooth time-periodic feedback solutions for nonholonomic motion planning," in Nonholonomic Motion Planning, Z. li and J. F. Canny, Eds. Springer New York, NY, 1993, pp. 53–108, https://doi.org/10.1007/978-1-4615-3176-0_3.
[113]P. Tsiotras, M. Corless, and J. M. Longuski, "A novel approach to the attitude control of axisymmetric spacecraft," Automatica, vol. 31, no. 8, pp. 1099-1112, 1995, https://doi.org/10.1016/0005-1098(95)00010-T.
[114]P. Tsiotras and J. Luo, "Stabilization and tracking of underactuated axisymmetric spacecraft with bounded control," IFAC Proceedings Volumes, vol. 31, no. 17, pp. 149-154, 1998, https://doi.org/10.1016/S1474-6670(17)40326-0.
[115]T. Tsiotras and A. Schleicher, "Detumbling and partial attitude stabilization of a rigid spacecraft under actuator failure," in AIAA Guidance, Navigation, and Control Conference and Exhibit; Dever, CO, USA, 2000, pp. 1–8, https://doi.org/10.2514/6.2000-4044.
[116]P. Tsiotras and V. Doumtchenko, "Control of spacecraft subject to actuator failures: State-of-the-art and open problems," Journal of the Astronautical Sciences, vol. 48, pp. 337-358, 2000, https://doi.org/10.1007/BF03546283.
[117]A. H. Bajodah, "Asymptotic perturbed feedback linearisation of underactuated Euler’s dynamics," International Journal of Control, vol. 82, no. 10, pp. 1856-1869, 2009, https://doi.org/10.1080/00207170902788613.
[118]A. Behal, D. Dawson, E. Zergeroglu, and Y. Fang, "Nonlinear tracking control of an underactuated spacecraft," Journal of Guidance, Control, and Dynamics, vol. 25, no. 5, pp. 979–984, 2002, https://doi.org/10.2514/2.4973.
[119]D. Casagrande, A. Astolfi, and T. Parisini, "Global asymptotic stabilization of the attitude and the angular rates of an underactuated non-symmetric rigid body," Automatica, vol. 44, no. 7, pp. 1781-1789, 2008, https://doi.org/10.1016/j.automatica.2007.11.022.
[120]S. P. Bhat and P. K. Tiwari, "Controllability of spacecraft attitude using control moment gyroscopes," IEEE Transactions on Automatic Control, vol. 54, no. 3, pp. 585-590, 2009, https://doi.org/10.1109/TAC.2008.2008324.
[121]H. Krishnan, M. Reyhanoglu, and H. McClamroch, "Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics," Automatica, vol. 30, no. 6, pp. 1023-1027, 1994, https://doi.org/10.1016/0005-1098(94)90196-1.
[122]G. C. Walsh, R. Montgomery, and S. S. Sastry, "Orientation control of the dynamic satellite," in American Control Conference - ACC '94, Baltimore, MD, USA, 1994, pp. 138–142, https://doi.org/10.1109/ACC.1994.751710.
[123]X. S. Ge, L. Q. Chen, and Y.Z. Liu, "Attitude control of underactuated spacecraft through flywheels motion using genetic algorithm with wavelet approximation," in 5th World Congress on Intelligent Control and Automation, Hangzhou, China, 2004, pp. 5466–5470, https://doi.org/10.1109/WCICA.2004.1343777.
[124]H. Gui, L. Jin, and S. Xu, "Small-time local controllability of spacecraft attitude using control moment gyros," Automatica, vol. 53, pp. 141-148, 2015, https://doi.org/10.1016/j.automatica.2014.12.047.
[125]N. M. Horri and P. Palmer, "Practical implementation of attitude-control algorithms for an underactuated satellite," Journal of Guidance, Control, and Dynamics, vol. 35, no. 1, pp 40–50, 2012, https://doi.org/10.2514/1.54075.
[126]O. J. Sordalen, O. Egeland, and C. Canudas de Wit, "Attitude stabilization with a nonholonomic constraint," in 31st Conference on Decision and Control, Tucson, AZ, USA, 1992, pp. 1610–1611, https://doi.org/10.1109/CDC.1992.371455.
[127]S. Kasai, H. Kojima, and M. Satoh, "Spacecraft attitude maneuver using two single-gimbal control moment gyros," Acta Astronautica, vol. 84, pp. 88-98, 2013, https://doi.org/10.1016/j.actaastro.2012.07.035.
[128]J. M. Godhavn and O. Egeland, "Attitude control of an underactuated satellite," in 34th IEEE Conference on Decision and Control New Orleans, LA, USA, 1995, pp. 3986–3987, https://doi.org/10.1109/CDC.1995.479227.
[129]S. Li and Y. P. Tian, "Exponential stabilization of the attitude of a rigid spacecraft with two controls," in American Control Conference, Anchorage, AK, USA, 2002, pp. 797–802, https://doi.org/10.1109/ACC.2002.1024912.
[130]P. Lucibello and G. Oriolo, "Robust stabilization of the angular velocity for an underactuated rigid spacecraft," IFAC Proceedings Volumes, vol. 31, no. 17, pp. 687-692, 1998, https://doi.org/10.1016/S1474-6670(17)40417-4.
[131]H. Shen and P. Tsiotras, "Time-optimal control of axisymmetric rigid spacecraft using two controls," Journal of Guidance, Control, and Dynamics, vol. 22, no. 5, pp. 682–694, 2012, https://doi.org/10.2514/2.4436.
[132]S. Kim and Y. Kirn, "Sliding mode stabilizing control law of underactuated spacecraft," in AIAA Guidance, Navigation, and Control Conference and Exhibit; Dever, CO, USA, 2000, Art. no. 4045, https://doi.org/10.2514/6.2000-4045.
[133]R. Eshaghi and F. Wang, "A Lyapunov-based fail-safe controller for an underactuated rigid-body spacecraft," in AIAA Guidance, Navigation, and Control Conference and Exhibit, Montreal, Canada, 2001, Art. no. 4212, https://doi.org/10.2514/6.2001-4212.
[134]F. Bacconi, D. Angeli, and E. Mosca, "Attitude control of asymmetric spacecrafts subject to actuator failures," in Conference on Control Applications, Istanbul, Turkey, 2003, pp. 474–479, https://doi.org/10.1109/CCA.2003.1223460.
[135]H. Ashrafiuon and R. S. Erwin, "Sliding control approach to underactuated multibody systems," in American Control Conference, Boston, MA, USA, 2004, pp. 1283–1288, https://doi.org/10.23919/ACC.2004.1386750.
[136]F. Terui, "Moon tracking attitude control experiment of a bias momentum micro satellite “μ-LabSat”," Transactions of the Japan Society for Aeronautical and Space Sciences, vol. 48, no. 159, pp. 28-33, 2005, https://doi.org/10.2322/tjsass.48.28.
[137]H. Ashrafiuon and R. S. Erwin, "Shape change maneuvers for attitude control of underactuated satellites," in American Control Conference, Portland, OR, USA, 2005, pp. 895–900, https://doi.org/10.1109/ACC.2005.1470073.
[138]H. Yang and Z. Wu, "Controllability study of the attitude control system for underactuated spacecraft," in 6th Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation, Beijing, China, 2006, Art. no. 635831, https://doi.org/10.1117/12.718053.
[139]M. A. Karami and F. Sassani, "Nonlinear attitude control of an underactuated spacecraft subject to disturbance torques," in American Control Conference, New York, NY, USA, 2007, pp. 3150–3155, https://doi.org/10.1109/ACC.2007.4283042.
[140]W. F. Dellinger and H. S. Shapiro, "Attitude control on two wheels and no gyros - The past, present, and future of the TIMED spacecraft," in AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, Hawaii, 2008, Art. no. 6258, https://doi.org/10.2514/6.2008-6258.
[141]C. Han and A. N. Pechev, "Time-varying nonlinear designs for underactuated attitude control with two reaction wheels," in 9th Biennial Conference on Engineering Systems Design and Analysis, Haifa, Israel, 2008, pp. 653-657, https://doi.org/10.1115/ESDA2008-59387.
[142]X. Ge and L. Chen, "Optimal reorientation of underactuated spacecraft using genetic algorithm with wavelet approximation," Acta Mechanica Sinica, vol. 25, pp. 547-553, 2009, https://doi.org/10.1007/s10409-009-0246-6.
[143]A. R. Mehrabian, S. Tafazoli, and K. Khorasani, "On the attitude recovery of an underactuated spacecraft using two control moment gyroscopes," in 48h Conference on Decision and Control (CDC) held jointly with 2009 28th Chinese Control Conference, Shanghai, China, 2009, pp. 1463–1470, https://doi.org/10.1109/CDC.2009.5399684.
[144]J. S. Hall, M. Romano, and R. Cristi, "Quaternion feedback regulator for large angle maneuvers of underactuated spacecraft," in American Control Conference, Baltimore, MD, USA, 2010, pp. 2867–2872, https://doi.org/10.1109/ACC.2010.5531481.
[145]Godard and K. D. Kumar, "Robust attitude stabilization of spacecraft subject to actuator failures," Acta Astronautica, vol. 68, no. 7-8, pp. 1242-1259, 2011, https://doi.org/10.1016/j.actaastro.2010.10.017.
[146]Y. Yoshimura, T. Matsuno, and S. Hokamoto, "Three dimensional attitude control of an underactuated satellite with thrusters," International Journal of Automation Technology, vol. 5, no. 6, pp. 892-899, 2011, https://doi.org/10.20965/ijat.2011.p0892.
[147]Y. Zhuang, H. Huang, and G. Ma, "Optimal trajectory generation of an asymmetric underactuated spacecraft based on orbital flatness," in International Conference on Mechatronics and Automation, Chengdu, China, 2012, pp. 327–331, https://doi.org/10.1109/ICMA.2012.6282863.
[148]Z. Yuan, X. Jianping, J. Jin, and Y. Jian, "Stabilization analysis and algorithm refactoring of underactuated small satellite using two wheels," in 25th Chinese Control and Decision Conference (CCDC), Guiyang, China, 2013, pp. 2314–2318, https://doi.org/10.1109/CCDC.2013.6561323.
[149]J. Huang, C. J. LI, G. F. MA, and G. Liu, "Generalised inversion based attitude control for underactuated spacecraft," Acta Automatica Sinica, vol. 39, no. 3, pp. 285-292, 2013, https://doi.org/10.1016/S1874-1029(13)60030-0.
[150]D. X. Wang, Y. H. Jia, L. Jin, F. G. Zhou, and S. Xu, "Hierarchical sliding-mode control for attitude stabilization of an underactuated spacecraft," Yuhang Xuebao/Journal of Astronautics, vol. 34, no. 1, pp. 17-24, 2013, https://doi.org/10.3873/j.issn.1000-1328.2013.01.003.
[151]J. R. Chaurais, H. C. Ferreira, J. Y. Ishihara, and R. A. Borges, "Attitude control of an underactuated satellite using two reaction wheels," Journal of Guidance, Control, and Dynamics, vol. 38, no. 10, pp. 2010-2018, 2015, https://doi.org/10.2514/1.G000145.
[152]Y. Katsuyama, T. Ibuki, K. Sekiguchi, and M. Sampei, "Attitude controllability analysis of an underactuated satellite with two reaction wheels and its control," in 54th Conference on Decision and Control (CDC), Osaka, Japan, 2015, pp. 3421-3426, https://doi.org/10.1109/CDC.2015.7402735.
[153]S. Daozhe, G. Yunhai, and F. Xiang, "Spacecraft line-of-sight nonlinear control using two wheels," in 10th International Conference on Intelligent Systems and Control (ISCO), Coimbatore, India, 2016, pp. 1-6, https://doi.org/10.1109/ISCO.2016.7726992.
[154]Y. Geng, D. Song, and R. Sun, "Inverse optimal stabilization of an underactuated spacecraft using two wheels," in 8th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC), Hangzhou, China, 2016, pp. 279–282, https://doi.org/10.1109/IHMSC.2016.270.
[155]Y. Yoshimura, T. Matsuno, and S. Hokamoto, "Global trajectory design for position and attitude control of an underactuated satellite," Transactions of the Japan Society For Aeronautical and Space Sciences, vol. 59, no. 3, pp. 107-114, 2016, https://doi.org/10.2322/tjsass.59.107.
[156]T. Fukaishi, K. Sekiguchi, and K. Nonaka, "Attitude control of two-wheel spacecraft based on dynamics model via hierarchical linearization," SICE Journal of Control, Measurement, and System Integration, vol. 10, no. 4, pp. 310-316, 2017, https://doi.org/10.9746/jcmsi.10.310.
[157]A. Zavoli, G. De Matteis, F. Giulietti, and G. Avanzini, "Single-Axis pointing of an underactuated spacecraft equipped with two reaction wheels," Journal of Guidance, Control, and Dynamics, vol. 40, no. 6, pp 1465–1471, 2017, https://doi.org/10.2514/1.G002182.
[158]H. Li, W. Yan, and Y. Shi, "Continuous-time model predictive control of under-actuated spacecraft with bounded control torques," Automatica, vol. 75, pp. 144-153, 2017, https://doi.org/10.1016/j.automatica.2016.09.024.
[159]A. Alikhani, "Passive fault-tolerant control of an underactuated re-entry capsule," Journal of Aerospace Technology and Management, vol. 9, no. 4, pp. 442-452, 2017, https://doi.org/10.5028/jatm.v9i4.771.
[160]J. Jin, "Attitude control of underactuated and momentum-biased satellite using state-dependent Riccati equation method," International Journal of Aeronautical and Space Sciences, vol. 20, pp. 204-213, 2019, https://doi.org/10.1007/s42405-018-0104-5.
[161]H. Kojima and P. M. Trivailo, "Adaptive time-delay estimated sliding mode control for a bias momentum satellite with two reaction wheels," Transactions of the Japan Society for Aeronautical and Space Sciences, vol. 62, no. 4, pp. 236-245, 2019, https://doi.org/10.2322/tjsass.62.236.
[162]H. MoradiMaryamnegari and A. M. Khoshnood, "Robust adaptive vibration control of an underactuated flexible spacecraft," Journal of Vibration and Control, vol. 25, no. 4, pp. 834-850, 2018, https://doi.org/10.1177/1077546318802431.
[163]H. S. Ousaloo, "Globally asymptotic three-axis attitude control for a two-wheeled small satellite," Acta Astronautica, vol. 157, pp. 17-28, 2019, https://doi.org/10.1016/j.actaastro.2018.11.05.
[164]Y. Zhuang, G. Ma, H. Huang, and C. Li, "Real-time trajectory optimization of an underactuated rigid spacecraft using differential flatness," Aerospace Science and Technology, vol. 23, no. 1, pp. 132-139, 2012, https://doi.org/10.1016/j.ast.2011.06.010.
[165]J. Zhang, K. Ma, and G. Meng, "Controllability analysis and attitude path planning of underactuated spacecraft systems," Aerospace Science and Technology, vol. 33, no. 1, pp. 76-81, 2014, https://doi.org/10.1016/j.ast.2014.01.003.
[166]C. Duan, Q. Hu, Y. Zhang, and H. Wu, "Constrained single-axis path planning of underactuated spacecraft," Aerospace Science and Technology, vol. 107, 2020, Art. no. 106345, https://doi.org/10.1016/j.ast.2020.106345.
[167]M. Alamir and F. Boyer, "Fast generation of attractive trajectories for a deficient satellite. application to feedback control design," IFAC Proceedings Volumes, vol. 34, no. 13, pp. 693-698, 2001, https://doi.org/10.1016/S1474-6670(17)39073-0.
[168]M. Aminsafaee and M. H. Shafiei, "A robust approach to stabilization of 2-DOF underactuated mechanical systems," Robotica, vol. 38, no. 12, pp. 2221-2238, 2020, https://doi.org/10.1017/S0263574720000053.
[169]S. Mobayen, S. Mostafavi, and A. Fekih, "Non-singular fast terminal sliding mode control with disturbance observer for underactuated robotic manipulators," IEEE Access, vol. 8, pp. 198067-198077, 2020, https://doi.org/10.1109/ACCESS.2020.3034712.
[170]R. Moradi, A. Alikhani, and M Fathi Jegarkandi, "Spacecraft attitude fault tolerant control based on multi-objective optimization," Journal of Theoretical and Applied Mechanics, vol. 58, no. 4, pp. 983-996, 2020, https://doi.org/10.15632/jtam-pl/125008.
[171]R. Nadafi and M. Kabganian, "Robust backstepping attitude tracking control of an underactuated spacecraft with saturation and time-variant perturbations," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 236, no. 3, pp. 502–516, https://doi.org/10.1177/09544100211015938.
[172]G. Chen and W. Huo, "Angular velocity stabilization of underactuated rigid satellites based on energy shaping," Journal of the Franklin Institute, vol. 359, no. 4, pp. 1558-1581, 2022, https://doi.org/10.1016/j.jfranklin.2022.01.001.
[173]L. Jin and Y. Li, "Model predictive control-based attitude control of under-actuated spacecraft using solar radiation pressure," Aerospace, vol. 9, no. 9, 2022, Art. no. 498, https://doi.org/10.3390/aerospace9090498.
[174]C. Liu, S. Chen, Y. Guo, and W. Wang, "Robust adaptive control for rotational deployment of an underactuated tethered satellite system," Acta Astronautica, vol. 203, pp. 65-77, 2023, https://doi.org/10.1016/j.actaastro.2022.11.025.
[175]C. Duan, Q. Hu, Y. Yang, and H. N. Wu, "Constrained control of underactuated spacecraft using artificial potentials," IEEE Transactions on Industrial Electronics, vol. 71, no. 11, pp. 14803-14812, 2024, https://doi.org/10.1109/TIE.2024.3366202.
[176]P. H. dos Santos and R. A. J. Chagas, "Satellite attitude control using extended model predictive control (EMPC) under actuator failures," Advances in Space Research, vol. 74, no. 3, pp. 1314-1326, 2024, https://doi.org/10.1016/j.asr.2024.05.010.
[177]Y. Lu, X. Wang, Y. Liu, and P. Huang, "Reinforcement learning-based finite time control for the asymmetric underactuated tethered spacecraft with disturbances," Acta Astronautica, vol. 220, pp. 218-229, 2024, https://doi.org/10.1016/j.actaastro.2024.04.014.
[178]M. Alger and A. de Ruiter, "Practical considerations using transverse function methods on underactuated reaction wheel controlled spacecraft," Acta Astronautica, vol. 228, pp. 101-120, 2025, https://doi.org/10.1016/j.actaastro.2024.11.046.
[179]X. Wu, S. Luo, C. Wei, and Y. Liao, "Observer-based fault-tolerant attitude tracking control for rigid spacecraft with actuator saturation and faults," Acta Astronaut, vol. 178, pp. 824-834, 2021, https://doi.org/10.1016/j.actaastro.2020.10.017.
[180]W. E. Dixon, A. Behal, D. M. Dawson, and S. P. Nagarkatti, "Underactuated systems. nonlinear," in Nonlinear Control of Engineering Systems, A Lyapunov-Based Approach, Control Engineering, Boston, MA: Birkhäuser, 2003, pp. 269–335. https://doi.org/10.1007/978-1-4612-0031-4_6.
[181]L. Cao, B. Xiao, and M. Golestani, "Robust fixed-time attitude stabilization control of flexible spacecraft with actuator uncertainty," Nonlinear Dynamics, vol. 100, pp. 2505-2519, 2020, https://doi.org/10.1007/s11071-020-05596-5.
[182]B. Xiao, L. Cao, S. Xu, and L. Liu, "Robust tracking control of robot manipulators with actuator faults and joint velocity measurement uncertainty," IEEE/ASME Transactions on Mechatronics, vol. 25, no. 3, pp. 1354-1365, 2020, https://doi.org/10.1109/TMECH.2020.2975117.
[183]B. Xiao, X. Wu, L. Cao, and X. Hu, "Prescribed time attitude tracking control of spacecraft with arbitrary disturbance," IEEE Transactions on Aerospace and Electronic Systems, vol. 58, no. 3, pp. 2531-2540, 2022, https://doi.org/10.1109/TAES.2021.3135372.
[184]M. R. Abedini and M. Abedi, "Design of a robust fault-tolerant control algorithm based on failure mode effects criticality analysis for a three-axis satellite," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 233, no. 1, pp. 91–110, 2017, https://doi.org/10.1177/0954410017727300.
[185]Y. Xia, Z. Zhu, M. Fu, and S. Wang, "Attitude tracking of rigid spacecraft with bounded disturbances," IEEE Transactions on Industrial Electronics, vol. 58, no. 2, pp. 647-659, 2011, https://doi.org/10.1109/TIE.2010.2046611.
[186]M. Heydari Shahna and M. Abedi, "An anti-unwinding finite time fault tolerant sliding mode control of a satellite based on accurate estimation of inertia moments," ISA Transactions, vol. 101, pp. 23-41, 2020, https://doi.org/10.1016/j.isatra.2020.01.034.
[187]Y. Qu, X. Zhong, F. Zhang, X. Tong, L. Fan, and L. Dai, "Robust disturbance observer-based fast maneuver method for attitude control of optical remote sensing satellites," Acta Astronautica, vol. 201, pp. 83-93, 2022, https://doi.org/10.1016/j.actaastro.2022.08.050.
[188]X. Zhao and M. R. Emami, "Adaptive underactuated orbit/attitude control for space debris rendezvous," in Aerospace Conference (50100), Big Sky, MT, USA, 2021, pp. 1-11, https://doi.org/10.1109/AERO50100.2021.9438440.
[189]G. E. M. Abro, S. A. Bin Mohd Zulkifli, and V. S. Asirvadam, "Dual-loop single dimension fuzzy-based sliding mode control design for robust tracking of an underactuated quadrotor craft," Asian Journal of Control, vol. 25, no. 1, pp. 144-169, 2022, https://doi.org/10.1002/asjc.2753.
[190]H. Tian, A. Li, Y. Wang, and C. Wang, "Underactuated attitude tracking control of tethered spacecraft for deployment and spin-up," Advances in Space Research, vol. 71, no. 11, pp. 4829-4842, 2023, https://doi.org/10.1016/j.asr.2023.01.052.
[191]K. L. Fetzer, S. G. Nersesov, and H. Ashrafiuon, "Trajectory tracking control of spatial underactuated vehicles," International Journal of Robust and Nonlinear Control, vol. 31, no. 10, pp. 4897-4916, 2021, https://doi.org/10.1002/rnc.5509.
[192]Z. Zheng, W. Huo, and Z. Wu, "Trajectory tracking control for underactuated stratospheric airship," Advances in Space Research, vol. 50, no. 7, pp. 906-917, 2012, https://doi.org/10.1016/j.asr.2012.06.020.
[193]X. Liu, Z. Meng, and Z. You, "Adaptive collision-free formation control for under-actuated spacecraft," Aerospace Science and Technology, vol. 79, pp. 223-232, 2018, https://doi.org/10.1016/j.ast.2018.05.040.
[194]P. Tsiotras and J. Luo, "Control of underactuated spacecraft with bounded inputs," Automatica, vol. 36, no. 8, pp. 1153-1169, 2000, https://doi.org/10.1016/S0005-1098(00)00025-X.
[195]A. Behal, D. Dawson, E. Zergeroglu, and Y. Fang, "Nonlinear tracking control of an underactuated spacecraft," Journal of Guidance, Control, and Dynamics, vol. 25, no. 5, pp. 979-984, 2002, https://doi.org/10.2514/2.4973.
[196]A. Frias, K. D. Kumar, and A. de Ruiter, "Robust nonlinear control of underactuated spacecraft using a single thruster," in 65th International Astronautical Congress, Toronto, Canada, 2014, pp. 4836–4844.
[197]W. Wang and J. Yinghong, "Stabilization of an under-actuated spacecraft," in 34th Chinese Control Conference (CCC), Hangzhou, China, 2015, pp. 5544–5548, https://doi.org/10.1109/ChiCC.2015.7260506.
[198]Y. H. Geng, D. Z. Song, S. Wang, and R. Sun, "Line-of-sight stabilization of an underactuated satellite controlled by wheels," Yuhang Xuebao/Journal Astronaut, vol. 38, no. 1, pp. 57–65, 2017.
[199]B. Wang, Z. Meng, and P. Huang, "Attitude control of towed space debris using only tether," Acta Astronautica, vol. 138, pp. 152-167, 2017, https://doi.org/10.1016/j.actaastro.2017.05.012.
[200]Q. M. Lam, "Robust and adaptive reconfigurable control for satellite attitude control subject to under-actuated control condition of reaction wheel assembly," Mathematics in Engineering, Science and Aerospace (MESA), vol. 9, no. 1, pp. 47–63, 2018.
[201]R. Nadafi and M. Kabganian, "Robust nonlinear attitude tracking control of an underactuated spacecraft under saturation and time-varying uncertainties," European Journal of Control, vol. 63, pp. 133-142, 2022, https://doi.org/10.1016/j.ejcon.2021.09.003.
[202]C. Jia, Z. Meng, and P. Huang, "Attitude control for tethered towing debris under actuators and dynamics uncertainty," Advances in Space Research, vol. 64, no. 6, pp. 1286-1297, 2019, https://doi.org/10.1016/j.asr.2019.06.027.
[203]H. Kojima, "Backstepping-based steering control for spacecraft attitude control using two-skewed control moment gyroscopes," Journal of Guidance, Control, and Dynamics, vol. 46, no. 1, pp. 80-96, 2023, https://doi.org/10.2514/1.G006661.
[204] M. Zarourati, M. Mirshams, and M. Tayefi, "Integrated vibration suppression-based attitude tracking control of a flexible satellite in rapid imaging maneuver," Aerospace Systems, 2025, https://doi.org/10.1007/s42401-025-00388-4.
 
دوره 18، شماره 2
1404
صفحه 83-119

  • تاریخ دریافت 08 بهمن 1403
  • تاریخ بازنگری 24 فروردین 1404
  • تاریخ پذیرش 25 فروردین 1404
  • تاریخ اولین انتشار 27 فروردین 1404