APPROXIMATE CALCULATION OF THE PROCESS CHARACTERISTICS OF THE UAV LANDING ON ROPE

Authors

  • N. F. Tupitsin National Aviation University
  • І. V. Chychkan Taras Shevchenko National University of Kyiv

DOI:

https://doi.org/10.18372/1990-5548.52.11872

Keywords:

Unmanned aerial vehicle landing, rope stretching, Hooke's law, unmanned aerial vehicle overload

Abstract

Analytical  expressions,  which  connected  of  the  unmanned  aerial  vehicle  parameters  and characteristics  of  landing's  rope,  are  obtained.  In  particular,  the  relationship  between  the  necessary length  of  rope  and  the  value  of  its  stretching  during  the  landing  of  the  unmanned  aerial  vehicle  is determined. Meanwhile, additional dampers for the rope are not considered. The mathematical model of the deceleration process of unmanned aerial vehicle during its landing on rope is based on Hooke's law and Newton's 2nd law. One of the main assumptions at the development of the mathematical model is that of  the  braking  of  the unmanned  aerial  vehicle  after  its  coupling  with  the  rope  occurs  with  constant acceleration.

Author Biographies

N. F. Tupitsin, National Aviation University

Aviation Computer-Integrated Complexes Department, Educational & Research Institute of Information and Diagnostic Systems

Candidate of Science (Engineering). Assosiate Professor

І. V. Chychkan, Taras Shevchenko National University of Kyiv

Department of Intellectual and Information systems

Candidate of Science (Physics and Mathematics). Associate professor

References

Device for landing of the UAV, by V. М. Sineglazov, N. F. Tupitsyn, and A. A. Udovenko. (2010, October 11). Patent Ukraine no. 53306, IPC В64С 25/00. (in Ukrainian)

System of landing of an aircraft on a rope, by V. V. Rednikov. Patent Russian Federation no. 43845, IPC B 64 F 1/02, 2005. (in Russian).

N. F. Tupitsyn, L. V. Tupitsyna, and A. S. Yurchenko, “Calculation of the characteristics of the landing device of an unmanned aerial vehicle.” Electronics and Control Systems. no. 3 (29), 2011,

Kyiv, NAU, pp. 90–94. (in Russian).

L. G. Loitsyansky and A. I. Lurie, Course of Theoretical Mechanics, vol. II. Moscow: Publisher

Tehn.-theor. Lit., 1955, 595 p. (in Russian).

http://stanok.guru/

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How to Cite

Tupitsin, N. F., & Chychkan І. V. (2017). APPROXIMATE CALCULATION OF THE PROCESS CHARACTERISTICS OF THE UAV LANDING ON ROPE. Electronics and Control Systems, 2(52), 67–71. https://doi.org/10.18372/1990-5548.52.11872

Issue

Vol. 2 No. 52 (2017)

Section

TRANSPORT SYSTEMS

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