Abstract. Quadrotor stability is one of the most topical researches worldwide. It is due to the simplicity, availability and cost of such platform. This miniature aerial vehicle is highly manoeuvrable, straight forward to use and to maintain. It can be deployed to perform wide variety of tasks. On the other hand, the quadrotor suffers from non-stability, which makes it unreliable, especially when flying on low speed, high altitude and in windy circumstances. This paper discusses the improvement of the quadrotor by adding a stabilizing mechanism working as a passive breaking system in sharp and spontaneous turns. The mechanism is described and simulated as a standalone module. The end result represents the determination of the stiffness coefficient of the stabilizing actuator using fuzzy logic controller.
IntroductionResearching and optimizing Unmanned Aerial Vehicles (UAVs) is very topical. It is due to the developed commercial potential of this market, which lead to their exploitation for civil tasks. Traditionally UAV are used in the military field. However, nowadays, UAVs are being deployed into cinematographic, rescue, exploration and delivery tasks. UAVs are classified according to their type, size and tasks designed for. A rotorcraft type such as quadrotor is affordable products, easy to operate and maintain and does not require supporting infrastructures. As a vertical take-off and landing UAV, the quadrotor can start from any place and land without any difficulties. The maneuverability of the quadrotor is a major benefit. This simple UAV is used for landscaping, scanning high-rise buildings and monitoring. On the other hand, the low flight range, fragile chassis in comparison to other UAVs, and its non-stability; especially when flying at high altitude or in windy circumstances minimize the tasks variety, where it can be deployed.Many researches concentrate on optimizing the control systems, construction materials, path planning algorithms and generation of adequate mathematical models of the quadrotor. Our contribution to this topic is not far from the worldwide tendency. This paper describes passive stabilization mechanism for the quadrotor. The mechanical components to realize the idea and the control scheme are disscissed in paragraph 3, simulations and results in paragraph 4. While the bibliographic review on the subject matter is addressed in paragraph 2.