Simulation of take-off and landing of unmanned quadrocopter from the sloping surface in automatical mode of flight

Authors

  • Богдан Благітко Ivan Franko National University o f Lviv , 1 Universytetska St.,79000, Lviv, Ukraine
  • Юрій Мочульський Ivan Franko National University o f Lviv , 1 Universytetska St.,79000, Lviv, Ukraine
  • Ігор Заячук Center of Mathematical Modelling of IAPMM

Keywords:

unmanned quadrocopter, altimeter, three-axis giroscope, tri-axial accelerometer, triangular magnetometer, management, Proportional-differential (PD) regulator

Abstract

The necessity of analyzing and modeling the processes of take-off of unmanned quadrocopter from
the sloping surface and its landing on it is substantiated. Using the developed mathematical
models describing the process of take-off and landing, the numerical experiment is performed. The
analysis of the data indicated the characteristics of the influence of the slope of start-landing
unmanned quadrocopter on process of its put to a given waypoint.

Фізико-математичне моделювання та інформаційні технології

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Published

2018-11-19

How to Cite

Благітко, Б., Мочульський, Ю., & Заячук, І. (2018). Simulation of take-off and landing of unmanned quadrocopter from the sloping surface in automatical mode of flight. PHYSICO-MATHEMATICAL MODELLING AND INFORMATIONAL TECHNOLOGIES, (24), 7–13. Retrieved from https://fmmit.lviv.ua/index.php/fmmit/article/view/36

Issue

No. 24 (2016): Physico-mathematical modeling and informational technologies, 2016, Issue 24

Section

Articles