The method of takeoff and landing uav with help springboard

N. F. Tupitsin, B. I. Dmitrenko, A. A. Ziganshin, I. A. Stepanenko

Abstract


The work presents new method takeoff and landing for the unmanned aerial vehicles with help special form of springboard. The calculation of constructive parameters of unmanned aerial vehicle at their application with springboard is carried. The constructive peculiarities of such springboard are analyzed also

Keywords


Unmanned aerial vehicle; take-off; landing; springboard; acceleration; velocity; length of fuselage

References


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Zhitnikov, E. D. Tilt-and-Takeoff Device/ Patent RU №2307770, IPC B64F1/06. Publ. 27.02.2005. (in Russian).

Hafer, K.; Sachs, G. Tech VTOL/ Translated from the German. Moscow: Mir, 1985. 376 p. (in Russian).

Samkov, A. V.; Silkov, V. I.; Tupitsyn, M. F. “Technique Calculation of UAV Kinematical Parameters at Take-off with Springboard.” IEEE 2nd International Conference “Actual Problems of Unmanned Air Vehicles Developments” Ukraine, Kyiv, October, 15-17, 2013. pp. 217–220.

Tupitsyn, M. F.; Tupitsyn, I. M. The takeoff and landing device of flying machine with help of springboard. Patent UA №94251, IPC B64F 1/00, B64C 25/00, Publ. 10.11.14.


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