The invention relates to the technical field of unmanned aerial vehicle design, in particular to an unmanned aerial vehicle
propeller definite reliability modeling method and
system, a medium and a program product. The method comprises the following steps: firstly, constructing a demand model, a
system context, a use case and an
activity diagram of an unmanned aerial vehicle
propeller based on SysML, and defining a mathematical function relationship of core performance parameters such as thrust, torque and rotating speed; then statistical fitting is carried out in combination with experimental data, a joint performance margin equation is constructed, a definite
reliability theory is introduced, and the reliability value of the
propeller is calculated through a standard normal cumulative
distribution function; and finally, carrying out constraint binding on the constraint equation and the
system structure model to realize dynamic response and model linkage under parameter change. According to the method, integration of reliability analysis in the MBSE model is realized, and the
automation degree, the evaluation precision and the
engineering application efficiency of reliability modeling of the propeller system are remarkably improved.