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Feedback control of vibrations in an extendible cantilever sweptback wing

  • Hyperbolic Control Systems
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Analysis and Optimization of Systems

Part of the book series: Lecture Notes in Control and Information Sciences ((LNCIS,volume 111))

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References

  1. R.L.Bislinghoff, H.Ashley and R.L.Halfman, Aeroelasticity, Addison-Wesley, Reading, Mass.

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  2. M.Goland and Y.L.Luke, "A study of the Bending-Torsion Aeroleastic Modes for Airplane Wings", J.Aeronautical Sciences, Vol.16, No.7, 1949.

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  3. P.K.C. Wang and J.D. Wei, "Vibrations in a Moving Flexible Robot Arm", J.Sound and Vibration, Vol.116, No.1, 1987, pp.149–160.

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  4. P.K.C. Wang and J.D. Wei, "Feedback Control of Vibrations in a Moving Flexible Robot Arm with Rotary and Prismatic Joints", Proc. International Conf. on Robotics and Automation, Raleigh, N.C. Mar. 1987, Vol.3, pp.1683–1689.

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  6. P.K.C.Wang, "Control of Distributed Systems with Time-Dependent Spatial Domains", in preparation.

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  7. P.K.C.Wang, "Feedback Control of Vibrations in an Extendible Cantilever Wing", Univ. of Calif. Los Angeles, Engr. Report ENG 87-36, September, 1987.

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A. Bensoussan J. L. Lions

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© 1988 Springer-Verlag

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Wang, P.K.C. (1988). Feedback control of vibrations in an extendible cantilever sweptback wing. In: Bensoussan, A., Lions, J.L. (eds) Analysis and Optimization of Systems. Lecture Notes in Control and Information Sciences, vol 111. Springer, Berlin, Heidelberg. https://doi.org/10.1007/BFb0042239

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  • DOI: https://doi.org/10.1007/BFb0042239

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-19237-4

  • Online ISBN: 978-3-540-39161-6

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