Design of Fail-Safe Quadrocopter Configuration

Деятельность: выступлениевыступление с устной презентацией


Unmanned aerial vehicles have become widespread in various fields of activity. In this article, we propose an approach to choosing performance characteristics of a quadrocopter, which provides a possibility to solve emergency landing problems. The key target characteristics for such a device are substantiated. The calculation methodology assumes the selection of commercially available components with the appropriate characteristics. For this purpose, the eCalc software was used. In the second part of the work, we propose a mathematical model describing the quadrocopter movement in emergency situations. This model allows us to create algorithms for solving control problems in various emergency situations. For implementation, the possibilities of MATLAB package were used. A numerical experiment is carried out to prove the efficiency of this approach.


Выступление с докладом
Период7 окт 20199 окт 2019
Название событияThe 13th International Symposium on Intelligent Distributed Computing : IDC 2019
Тип мероприятияконференция
Номер конференции13
МестонахождениеСанкт-Петеррбург, Российская Федерация
Степень признанияМеждународная

Ключевые слова

  • quadrocopter
  • control
  • fail-safe configuration