The method of takeoff and landing uav with help springboard

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


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


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


Calco, I. P. Aircraft Takeoff Method/ Patent RU №2247059. IPC В 64 D 1/02, Publ. 23.04.2003. (in Russian).

Douglas Barrie “Russia and Israel prepare for dogfiight over Chinise missile” in FLIGHT INTERNATIONAL 24-30 September 1997.

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.

Full Text: PDF


  • There are currently no refbacks.

Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivs 3.0 Unported License.