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Dynamic flight stability of a model dronefly in vertical flight

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Abstract

The dynamic flight stability of a model dronefly in hovering and upward flight is studied. The method of computational fluid dynamics is used to compute the stability derivatives and the techniques of eigenvalue and eigenvector used to solve the equations of motion. The major finding is as following. Hovering flight of the model dronefly is unstable because of the existence of an unstable longitudinal and an unstable lateral natural mode of motion. Upward flight of the insect is also unstable, and the instability increases as the upward flight speed increases. Inertial force generated by the upward flight velocity coupled with the disturbance in pitching angular velocity is responsible for the enhancement of the instability.

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Authors and Affiliations

  1. Institute of Fluid Mechanics, Beijing University of Aeronautics & Astronautics, 100191, Beijing, China

    Chong Shen & Mao Sun

Authors
  1. Chong Shen
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  2. Mao Sun
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Correspondence to Mao Sun.

Additional information

The project was supported by the National Natural Science Foundation of China (11232002).

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Shen, C., Sun, M. Dynamic flight stability of a model dronefly in vertical flight. Acta Mech Sin 30, 828–838 (2014). https://doi.org/10.1007/s10409-014-0110-1

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  • DOI: https://doi.org/10.1007/s10409-014-0110-1

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