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SCIENCE CHINA Information Sciences, Volume 62, Issue 1: 010208(2019) https://doi.org/10.1007/s11432-018-9577-3

Control and dynamics analysis for miniature autogyro and compound autogyro

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  • ReceivedJun 27, 2018
  • AcceptedJul 16, 2018
  • PublishedDec 14, 2018

Abstract

There is no abstract available for this article.


Acknowledgment

This work was supported by AVIC Chengdu Aircraft Industrial (Group) Co. Ltd., Fundamental Research Funds for the Central Universities (Grant No. YWF-18-BJ-Y-190), and the Aeronautical Science Foundation of China (Grant No. 20175851032).


References

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  • Figure 1

    (Color online) (a) Roll step response; (b) pitch step response; (c) short takeoff (compound autogyro); (d) short landing (pure autogyro); (e) thrust command given at different airspeeds; (f) rotor rotation speed at different airspeeds.

  • Table 1   Aircraft parameters
    Parameter Unit Value
    Mass kg 1.980
    Length m 1.223
    Rotor diameter m 1.08
    Number of rotor blades 3
    Blade length m 0.518
    Blade chord length m 0.05
    Blade airfoil Clark Y (estimated)
    Collective pitch $^\circ~$ 0
    Fixed wing span m 0.74
    Fixed wing chord m 0.11
    Fixed wing airfoil Selig S3010
    Max thrust kg 1.0 (approximated)

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