4.8 Article

Vibration Control for Spatial Aerial Refueling Hoses With Bounded Actuators

Journal

IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS
Volume 68, Issue 5, Pages 4209-4217

Publisher

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TIE.2020.2984442

Keywords

Hoses; Vibrations; Mechanical systems; Actuators; Control design; Backstepping; Boundary control; distributed parameter system (DPE); flexible hose; rate and magnitude-bounded actuator

Funding

  1. China Postdoctoral Science Foundation [2019M660463]
  2. Fundamental Research Funds for the China Central Universities of USTB [FRF-IDRY-19-024, FRF-TP-19-001B2]
  3. Beijing Top Discipline for Artificial Intelligent Science and Engineering of USTB
  4. National Natural Science Foundation of China [61803109]
  5. Science and Technology Planning Project of Guangzhou City [201904010494]
  6. Hong Kong government [11210719]
  7. National Research Foundation of Korea (NRF) - Korea government (Ministry of Science and ICT) [NRF-2020R1A2C1005449]

Ask authors/readers for more resources

This article presents a control scheme for stabilizing a vibrating flexible hose used for aerial refueling subject to bounded actuators. The dynamical model of the hose system is captured by partial differential equations, with a novel boundary control law proposed to dampen the vibration. The control scheme is devised using the backstepping approach and verified for stability using the Lyapunov criterion, with simulation results evaluating its validity.
This article presents a control scheme for stabilizing a vibrating flexible hose used for aerial refueling subject to bounded actuators for the rate and magnitude. A dynamical model of hose systems is captured by partial differential equations (PDEs). Based on the PDE model, a novel boundary control law is proposed to dampen the flexible hose's vibration. The backstepping approach is utilized to devise the control scheme, with the bounded input magnitude and derivative handled by adopting the smooth hyperbolic tangent function. The Lyapunov criterion is exploited to demonstrate the stability of the controlled system. Finally, simulation results are used to evaluate the validity of the derived scheme.

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