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This article is concerned with parameters identification problems and computer modeling of thrust generation subsystem for small unmanned aerial vehicles (UAV) quadrotor type. In this paper approach for computer model generation of dynamic process of thrust generation subsystem that consists of fixed pitch propeller, EC motor and power amplifier, is considered. Due to the fact that obtainment of aerodynamic...
The article is devoted to the parameter's identification of the propulsion subsystem and control system design for small unmanned aerial vehicles (UAV) helicopter type. Parameter's identification is realized with a special test rig developed by authors of the project, the description of which is presented in the article. The designed test rig application is the parameter's identification of power...
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