نوع مقاله : علمی- ترویجی
نویسندگان
1 دانشجوی دکترا، دانشکده مهندسی مکانیک، گروه هوافضا، دانشگاه تربیت مدرس، تهران، ایران.
2 دانشیار، دانشکده مهندسی مکانیک، گروه هوافضا، دانشگاه تربیت مدرس، تهران، ایران.
چکیده
در این مقاله، مسئله ملاقات و اتصال مداری به‌عنوان یک المان کلیدی و با اهمیت که دارای کاربردهای اساسی و مهم نیز در حوزه فضایی بوده، مورد مطالعه قرار گرفته است. در نتیجه هدف اصلی این مقاله بیان کلیات و بخش‌های مهم یک مأموریت ملاقات و اتصال است. همچنین، اهمیت و نمونه‌هایی از کاربرد مسئله معرفی و سپس مراحل مشترک در یک مأموریت ملاقات و اتصال مداری، رویکردهای حل مسئله و روش‌های پرکاربرد بیان شده‌اند. یک بخش با اهمیت در مأموریت ملاقات و اتصال کنترل سامانه است. بنابراین، کنترل‌کننده‌های پرکاربرد در این مسئله و برخی از مزایا و معایب آن‌ها بیان شده و کنترل همزمان موقعیت و وضعیت نیز به‌عنوان یک چالش مهم مورد بررسی قرار گرفته است. در ادامه برخی از رویکردها و سنسورهای متداول ناوبری در یک مسئله ملاقات و اتصال مداری معرفی شده و در نهایت مثال‌ها و نمونه‌هایی از تجهیزات آزمایشگاهی، به‌عنوان یک ابزار مهم ارائه شده‌اند.
کلیدواژه‌ها
موضوعات
[1] W. Fehse, Automated rendezvous and docking of spacecraft vol. 16: Cambridge university press, 2003.
[2] E. Seedhouse, SpaceX's Dragon: America's Next Generation Spacecraft: Springer, 2015.
[3] Y. Xie, C. Chen, T. Liu, and M. Wang, Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods: Springer Nature, 2021.
[4] A. Petit, E. Marchand, and K. Kanani, "Vision-based space autonomous rendezvous: A case study," in 2011 IEEE/RSJ International Conference on Intelligent Robots and Systems, 2011, pp. 619-624.
[5] J. C. Morris, "Automated spacecraft docking using a vision-based relative navigation sensor," Texas A & M University, 2010.
[6] C. M. Jewison, "Guidance and control for multi-stage rendezvous and docking operations in the presence of uncertainty," Massachusetts Institute of Technology, 2017.
[7] Q. Wang, B. Zhou, and G.-R. Duan, "Robust gain scheduled control of spacecraft rendezvous system subject to input saturation," Aerospace Science and Technology, vol. 42, pp. 442-450, 2015.
[8] H. Taei and P. Shokrolahi, "Applying multi-objective optimization approaches to design an optimal controller for orbital docking by consideration of actuators dynamics and comparing results," Journal of Space Science and Technology, vol. 13, pp. 85-96, 2020.
[9] M. Navabi and M. Reza Akhloumadi, "Nonlinear optimal control of orbital rendezvous problem for circular and elliptical target orbit," Modares Mechanical Engineering, vol. 15, pp. 132-142, 2016.
[10] J. TSCHAUNER, "Elliptic orbit rendezvous," AIAA journal, vol. 5, pp. 1110-1113, 1967.
[11] A. Imani and B. Beigzadeh, "Robust control of spacecraft rendezvous on elliptical orbits: Optimal sliding mode and backstepping sliding mode approaches," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 230, pp. 1975-1989, 2016.
[12] E. Capello, E. Punta, F. Dabbene, G. Guglieri, and R. Tempo, "Sliding-mode control strategies for rendezvous and docking maneuvers," Journal of Guidance, Control, and Dynamics, vol. 40, pp. 1481-1487, 2017.
[13] K. Xia and W. Huo, "Disturbance observer based fault-tolerant control for cooperative spacecraft rendezvous and docking with input saturation," Nonlinear Dynamics, vol. 88, pp. 2735-2745, 2017.
[14] S. Segal and P. Gurfil, "Effect of kinematic rotation-translation coupling on relative spacecraft translational dynamics," Journal of Guidance, Control, and Dynamics, vol. 32, pp. 1045-1050, 2009.
[15] W. Lu, Y. Geng, X. Chen, and F. Zhang, "Relative position and attitude coupled control for autonomous docking with a tumbling target,”" International Journal of Control and Automation, vol. 4, pp. 1-22, 2011.
[16] D. Lee, H. Bang, E. A. Butcher, and A. K. Sanyal, "Kinematically coupled relative spacecraft motion control using the state-dependent Riccati equation method," Journal of Aerospace Engineering, vol. 28, p. 04014099, 2015.
[17] W. Gao, X. Zhu, M. Zhou, and Q. Jiang, "ADRC law of spacecraft rendezvous and docking in final approach phase," Cybernetics and Systems, vol. 47, pp. 236-248, 2016.
[18] M. E. Polites, "Technology of automated rendezvous and capture in space," Journal of spacecraft and Rockets, vol. 36, pp. 280-291, 1999.
[19] J. Bowen, M. Villa, and A. Williams, "Cubesat based rendezvous, proximity operations, and docking in the CPOD mission," 2015.
[20] C. Pirat, F. Ankersen, R. Walker, and V. Gass, "Vision based navigation for autonomous cooperative docking of CubeSats," Acta Astronautica, vol. 146, pp. 418-434, 2018.
[21] D. Fourie, B. Tweddle, S. Ulrich, and A. Saenz Otero, "Vision-based relative navigation and control for autonomous spacecraft inspection of an unknown object," in AIAA guidance, navigation, and control (GNC) conference, 2013, p. 4759.
[22] N. K. Philip and M. Ananthasayanam, "Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft," Acta Astronautica, vol. 52, pp. 511-522, 2003.
[23] P. Huang, L. Chen, B. Zhang, Z. Meng, and Z. Liu, "Autonomous rendezvous and docking with nonfull field of view for tethered space robot," International Journal of Aerospace Engineering, vol. 2017, 2017.
[24] M. Navabi and M. R. Akhlomadi, "Nonlinear optimal control of space docking and rendezvous problem," Journal of Space Science and Technology, vol. 8, 2015.
[25] J. Liang and O. Ma, "Angular velocity tracking for satellite rendezvous and docking," Acta Astronautica, vol. 69, pp. 1019-1028, 2011.
[26] S. He, W. Wang, D. Lin, and H. Lei, "Robust output feedback control design for autonomous spacecraft rendezvous with actuator faults," Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, vol. 230, pp. 578-587, 2016.
[27] Q. Li, J. Yuan, B. Zhang, and C. Gao, "Model predictive control for autonomous rendezvous and docking with a tumbling target," Aerospace Science and Technology, vol. 69, pp. 700-711, 2017.
[28] D.-R. Lee and H. Pernicka, "Optimal control for proximity operations and docking," International Journal of Aeronautical and Space Sciences, vol. 11, pp. 206-220, 2010.
[29] J. Nandagopal and R. Lethakumari, "Optimal control of Spacecraft Docking System using integral LOR controller," in 2015 International Conference on Technological Advancements in Power and Energy (TAP Energy), 2015, pp. 18-22.
[30] Y. Han, J. D. Biggs, and N. Cui, "Adaptive fault-tolerant control of spacecraft attitude dynamics with actuator failures," Journal of Guidance, Control, and Dynamics, vol. 38, pp. 2033-2042, 2015.
[31] L. Sun and Z. Zheng, "Adaptive sliding mode control of cooperative spacecraft rendezvous with coupled uncertain dynamics," Journal of Spacecraft and Rockets, vol. 54, pp. 652-661, 2017.
[32] D. Ye, W. Lu, and Z. Mu, "Compound control for autonomous docking to a three-axis tumbling target," Transactions of the Institute of Measurement and Control, vol. 41, pp. 911-924, 2019.
[33] Q. Hu, X. Shao, and W.-H. Chen, "Robust fault-tolerant tracking control for spacecraft proximity operations using time-varying sliding mode," IEEE Transactions on Aerospace and Electronic Systems, vol. 54, pp. 2-17, 2017.
[34] Y. Wang and H. Ji, "Integrated relative position and attitude control for spacecraft rendezvous with ISS and finite-time convergence," Aerospace Science and Technology, vol. 85, pp. 234-245, 2019.
[35] Y. Liu, H. Zhang, S. Zhang, H. Li, C. Li, J. Ren, et al., "Minimum-learning-parameter-based fault-tolerant control for spacecraft rendezvous with unknown inertial parameters," IEEE Access, vol. 8, pp. 151487-151499, 202.
[36] M. AlandiHallaj and N. Assadian, "Soft landing on an irregular shape asteroid using multiple-horizon multiple-model predictive control," Acta Astronautica, vol. 140, pp. 225-234, 2017.
[37] O. Iskender, K. V. Ling, and V. Dubanchet, "Constraints tightening approach towards model predictive control based rendezvous and docking with uncooperative targets," in 2018 European Control Conference (ECC), 2018, pp. 380-385.
[38] R. Vazquez, F. Gavilan, and E. F. Camacho, "Model predictive control for spacecraft rendezvous in elliptical orbits with on/off thrusters," IFAC-PapersOnLine, vol. 48, pp. 251-256, 2015.
[39] Y. Shtessel, C. Edwards, L. Fridman, and A. Levant, "Sliding mode control and observation", Springer, Birkhäuser New York, NY, USA, 2014.
[40] L. Wang, "Model predictive control system design and implementation using MATLAB", Springer Science & Business Media, London, UK, 2009.
[41] W. Zhou, H. Wang, G. Tang, and S. Guo, "Inverse simulation system for manual-controlled rendezvous and docking based on artificial neural network", Advances in Space Research, vol. 58, no. 6, pp. 938-949, 2016.
[42] J. Leitner, C. Ampatzis, and D. Izzo, "Evolving ANNs for spacecraft rendezvous and docking", InProceedings of the 10th International Symposium on Artificial Intelligence- Robotics and Automation in Space- i-SAIRAS- European Space Agency (ESA), Sapporo, Japan, pp. 386-393, 2010.
[43] J. Ho and N.H. McClamroch, "A spacecraft docking problem: position and orientation estimation using a computer vision approach", American Control Conference, Boston, USA, 1991
[44] Z. Wei, H. Wen, H. Hu, and D. Jin, "Ground experiment on rendezvous and docking with a spinning target using multistage control strategy", Aerospace Science and Technology, vol. 104, p. 105967, 2020
[45] S. Shi, L. Yang, J. Lin, Y. Ren, S. Guo, and J. Zhu, "Omnidirectional angle constraint based dynamic six-degree-of-freedom measurement for spacecraft rendezvous and docking simulation", Measurement Science and Technology, vol. 29, no. 4, p. 045005, 2018.
[46] M. Sabatini, G.B. Palmerini, and P. Gasbarri, "A testbed for visual based navigation and control during space rendezvous operations", Acta Astronautica, vol. 117, pp.184-196, 2015.
[47] R.I. Zappulla, H. Park, J. Virgili-Llop, and M. Romano, "Experiments on autonomous spacecraft rendezvous and docking using an adaptive artificial potential field approach", n Proceedings of the 26th AAS/AIAA Space Flight Mechanics Meeting, Napa, CA, USA, 14–18 February 2016.
)