Autors: Azadmanesh M., Todorov M., Georgiev, K. K.
Title: Leveraging fuzzy logic for an asteroid mission: Introducing a new fuzzy algorithm
Keywords:

Abstract: New Fuzzy Controller is introduced in this paper and tested on the asteroid landing problem. The controller takes the system modes' distance from an intended sliding surface and effectively adjusts the parameters that control the input functions. It is combined with two different sliding mode controllers and compared with another fuzzy system which inspired the New Fuzzy algorithm. The New Fuzzy controller is a logarithm-based approach that successfully smooths the convergence procedure and effectively eliminates the chattering problem that comes with the sliding mode controllers. The position and velocity tracking errors are obtained, and the results show that the New Fuzzy controller does the tracking more accurately and efficiently than the formerly used approach and manages to land the vehicle smoothly and precisely.

References

  1. Y. Li, H. Wang, B. Zhao, K. Liu, "Adaptive fuzzy sliding mode control for the probe soft landing on the asteroids with weak gravitational field," Mathematical Problems in Engineering 2015, 582948 (2015).
  2. Y.-n. Yang, J. Wu, and W. Zheng, "Trajectory tracking for an autonomous airship using fuzzy adaptive sliding mode control," Journal of Zhejiang University SCIENCE C 13, pp. 534-543 (2012). 10.1631/jzus.C1100371
  3. H. T. Cui, X. Y. Shi, P. Y. Cui, "Guidance and control law for soft landing asteroid," Journal of Flight Dynamics 20, pp. 35-38 (2002).
  4. G. Zhang, S. Qiu, and F. Wang, "Adaptive fuzzy fault-tolerant control of flexible spacecraft with rotating appendages," International Journal of Fuzzy Systems 25, pp. 326-337 (2023).
  5. P. Cui, S. Zhu, and H. Cui, "Autonomous impulse maneuver control method for soft landing on small bodies," Journal of Astronautics 29, pp. 511-516 (2008).
  6. J. Carson, B. Acikmese, R. Murray and D. MacMynowski, "Robust model predictive control with a safety mode: applied to small-body proximity operations," in AIAA Guidance, Navigation and Control Conference and Exhibit (18-21 August 2008, Honolulu, Hawaii).
  7. Q. Lan, et al., "Finite-time soft landing on asteroids using nonsingular terminal sliding mode control," Transactions of the Institute of Measurement and Control 36 (2), pp. 216-223 (2014).
  8. H. Yang, X. Bai, and H. Baoyin, "Finite-time control for asteroid hovering and landing via terminal sliding-mode guidance," Acta Astronautica 132, pp. 78-89 (2017).
  9. H. Zenk, H. Senol, and F. Güner, "Lunar excursion module landing control system design with P, PI and PID controllers," Karadeniz Fen Bilimleri Dergisi 9 (2), pp. 390-405 (2019). 10.31466/kfbd.647211
  10. M. Azadmanesh, J. Roshanian, and M. Hassanalian, "Fast terminal sliding mode control for the soft landing of a space robot on an asteroid considering a barycentric gravitational model," Journal of Aerospace Science and Technology 16 (1), pp. 66-76 (2023).
  11. M. Azadmanesh, J. Roshanian, and M. Hassanalian, "A fuzzy fast terminal approach for tracking a probe around an asteroid," Journal of Aerospace Science and Technology 16 (2), pp. 1-10 (2023).
  12. A. Shornikov, and O. Starinova, "Simulation of controlled motion in an irregular gravitational field for an electric propulsion spacecraft," in 7th International Conference on Recent Advances in Space Technologies (RAST) (Istanbul, Turkey, 2015), (IEEE, 2015), pp. 771-776.
  13. A. Shornikov, and O. Starinova, "Boundary problem solution algorithm for the task of controlled spacecraft motion in irregular gravitational field of an asteroid," Procedia Engineering 185, pp. 411-417 (2017). 10.1016/j.proeng.2017.03.323
  14. M. Azadmanesh, et al., "Improved fast terminal sliding mode control for an extraterrestrial lander," in AIAA Aviation Forum and Ascend (29 July-2 August 2024, Las Vegas, Nevada).
  15. M. Azadmanesh, et al., "Achieving synchronized angular velocities in chaotic satellite systems: A novel controller ", in AIAA Aviation Forum and Ascend (29 July-2 August 2024, Las Vegas, Nevada).
  16. M. Azadmanesh, et al., "Parameter estimation based on prediction error for the soft-landing problem in micro-gravity," in AIAA Aviation Forum and Ascend (29 July-2 August 2024, Las Vegas, Nevada).
  17. S. M. T. Bathaee, and M. J. Harandi, "Decentralized load frequency control of multi-area power systems using combined variable structure and fuzzy logic controller," IFAC Proceedings Volumes 30, pp. 493-498 (1997).
  18. M. Azadmanesh, J. Roshanian, and M. Hassanalian, "On the importance of studying asteroids: A comprehensive review," Progress in Aerospace Sciences, 100957 (2023).
  19. M. Azadmanesh, et al., "Synchronization of angular velocities of chaotic leader-follower satellites using a novel integral terminal sliding mode controller," Aerospace Science and Technology 150, 109211 (2024). 10.1016/j.ast.2024.109211

Issue

AIP Conference Proceedings, vol. 3339, pp. 020004, 2025, United States, https://doi.org/10.1063/5.0298633

Copyright AIP Publishing

Вид: публикация в национален форум с межд. уч., публикация в издание с импакт фактор, публикация в реферирано издание, индексирана в Scopus