LINEAR ACTIVE DISTURBANCE REJECTION CONTROL WITH A HIGHER ORDER SLIDING MODE OBSERVER APPLIED TO A CART INVERTED PENDULUM, 220-227.

Suhail A. Suhail,∗ Mohammad A. Bazaz,∗ and Shoeb Hussain∗

References

  1. [1] H.O. Wang, K. Tanaka, and M.F. Griffin, An approach tofuzzy control of nonlinear systems: Stability and design issues,IEEE Transactions on Fuzzy Systems, 4, 1996, 14–23.
  2. [2] J.J. Wang, Stabilization and tracking control of X-Z invertedpendulum based on PID controllers, Proceedings of the 34thChinese Control Conference, Hangzhou, China, 2015, 4204–4207.
  3. [3] D. Chatterjee, A. Patra, and H.K. Joglekar, Swing-up andstabilization of a cart-pendulum system under restricted carttrack length, System & Control Letters, 47(4), 2002, 355–364.
  4. [4] L. Magni, R. Scattolini, and K. Astrom, Global stabilizationof the inverted pendulum using model predictive control,Proceedings of the 15th IFAC World Congress, 15, 2002, 590–595.
  5. [5] C.W. Anderson, Learning to control an inverted pendulumusing neural networks, IEEE Control Systems Magazine, 9,1989, 31–37.
  6. [6] M. Cacciola, F.C. Morabito, D. Polimeni, and M. Versaci,Fuzzy characterization of flawed metallic plates with Eddycurrent tests, Progress in Electromagnetics Research, 72, 2007,241–252.
  7. [7] M. Cacciola, F. La Foresta, F.C. Morabito, and M. Versaci,Advanced use of soft computing and Eddy current test toevaluate mechanical integrity of metallic plates, NDT & EInternational, 40(5), 2007, 357–362.
  8. [8] M. Cacciola, S. Calcagno, G. Megali, F.C. Morabito, D. Pelli-cano , and M. Versaci, FEA design and misfit minimization forin-depth flaw characterization in metallic plates with Eddy cur-rent nondestructive testing, IEEE Transactions on Magnetics,45(3), 2009, 1506–1509.
  9. [9] E. Yazdi and R. Nagamune, Robust finite-time tracking withswitched controllers, Control and Intelligent Systems, 40(3),2012. doi: 10.2316/Journal.201.2012.3.201-2367
  10. [10] J.Q. Han, From PID to active disturbance rejection control,IEEE Transactions on Industrial Electronics, 56(3), 2009, 1–7.
  11. [11] S. Jiao, D. Liu, and X. Zheng, Attitude control of quad-copter based on self-tuning linear active disturbance rejec-tion, Mechatronic Systems and Control, 48(2), 2020. doi:10.2316/J.2020.201-0022
  12. [12] H. Jiang, Q. Chang, Y. Wang, and X. Xie, Optimizationof the active disturbance rejection control of a four-rotoraircraft, Mechatronic Systems and Control, 48(2), 2020. doi:10.2316/J.2020.201-0017
  13. [13] R. Parvathy, A. Daniel, and C. Noufal, Analysis of extended-state-observer and active-disturbance-rejection control in thespeed control Of DC motor system, Mechatronic Systems andControl, 47(2), 2019. doi: 10.2316/J.2019.201-2952
  14. [14] Z.Q. Gao, Scaling and bandwidth-parameterization based con-troller tuning, Proceedings of the 2003 American Control Con-ference, Denver, Colorado, USA, 2003, 4989–4996.
  15. [15] X. Chen, D. Li, Z. Gao, and C. Wang, Tuning method forsecond-order active disturbance rejection control, Proceedingsof the 30th Chinese Control Conference, Yantai, 2011, 6322–6327.
  16. [16] S.A. Suhail, M.A. Bazaz, and S. Hussain, Altitude and attitudecontrol of a quadcopter using linear active disturbance rejectioncontrol, 2019 International Conference on Computing, Powerand Communication Technologies (GUCON), NCR New Delhi,India, 2019, 281–286.
  17. [17] C. Dai, J. Yang, Z. Wang, and S. Li, Universal active dis-turbance rejection control for non-linear systems with multi-ple disturbances via a high-order sliding mode observer, IETControl Theory & Applications, 11(8), 2017, 1194–1204.
  18. [18] A. Ghosh, T.R. Krishnan, and B. Subudhi, Robustproportional-integral-derivative compensation of an invertedcartpendulum system: An experimental study, IET ControlTheory & Applications, 6(8), 2012, 1145–1152.
  19. [19] J. Yang, J.Y. Su, S.H. Li, et al., High-order mismatcheddisturbance compensation for motion control systems via acontinuous dynamic sliding mode approach, IEEE Transactionson Industrial Informatics, 10(1), 2014, 604–614.

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