Project for a reconnaissance unmanned aerial vehicle

Abstract

The paper presents the process of designing an unmanned Micro class aircraft, from the analysis of the dynamically developing market and the condition of the Polish Armed Forces to construction of objects and flight test. The possibilities and limitations of using miniature UAVs on the modern battlefield were determined. For the designed UAV the propulsion was selected based on tests carried out on the engine test bench. The avionics equipment was selected based on components readily available on the market. The object was then made and inspected in flight. During the flight tests, the aircraft performance was verified and compared with the assumptions. It has been shown that the developed object is able to fulfill the reconnaissance tasks entrusted to it, while maintaining the assumed simplicity of construction and low cost of execution and service.

Dynamical system design of an air-ground amphibious individual unmanned aerial vehicle

“…Table 1 shows the design and selection results. Choose an altitude of 20m and a temperature of 25℃, bring the parameters of the power components into the overall power system model, and calculate the performance [10] , as shown in Table 2:…”