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Bilateral coordinate boundary adaptive control for a helicopter lifting system with backlash-like hysteresis

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References

  1. Fusato D, Guglieri G, Celi R. Flight dynamics of an articulated rotor helicopter with an external slung load. J Am Helicopter Soc, 2001, 46: 3–13

    Article  Google Scholar 

  2. Adams C J, Potter J, Singhose W. Input-shaping and model-following control of a helicopter carrying a suspended load. J Guid Control Dyn, 2015, 38: 94–105

    Article  Google Scholar 

  3. Chen M, Ren Y, Liu J. Antidisturbance control for a suspension cable system of helicopter subject to input nonlinearities. IEEE Trans Syst Man Cybern Syst, 2018, 48: 2292–2304

    Article  Google Scholar 

  4. He W, Nie S X, Meng T T, et al. Modeling and vibration control for a moving beam with application in a drilling riser. IEEE Trans Contr Syst Technol, 2017, 25: 1036–1043

    Article  Google Scholar 

  5. Meng D, Liu H, Li Y, et al. Vibration suppression of a large flexible spacecraft for on-orbit operation. Sci China Inf Sci, 2017, 60: 050203

    Article  Google Scholar 

  6. Su C Y, Stepanenko Y, Svoboda J, et al. Robust adaptive control of a class of nonlinear systems with unknown backlash-like hysteresis. IEEE Trans Automat Contr, 2000, 45: 2427–2432

    Article  MathSciNet  MATH  Google Scholar 

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Acknowledgements

This work was supported in part by National Natural Science Foundation of China (Grant No. 61533008), Aeronautical Science Foundation of China (Grant No. 20165752049), and Jiangsu Natural Science Foundation of China (Grant No. BK20171417).

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Authors and Affiliations

  1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 211100, China

    Yong Ren, Mou Chen & Jianye Liu

Authors
  1. Yong Ren
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  2. Mou Chen
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  3. Jianye Liu
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Corresponding author

Correspondence to Mou Chen.

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Ren, Y., Chen, M. & Liu, J. Bilateral coordinate boundary adaptive control for a helicopter lifting system with backlash-like hysteresis. Sci. China Inf. Sci. 63, 119203 (2020). https://doi.org/10.1007/s11432-018-9636-3

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  • DOI: https://doi.org/10.1007/s11432-018-9636-3

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