This paper presents a kind of simulation program of aero-generator, that inverter adopts a computer-controlled manner to simulate actual working features of aero-generator, based on test platform status of aero-generator. And design of the structure of simulation system , analyze the working principle of aero-generator, and then set up simulation model of three-stage brushless aero-generator under SIMULINK. Finally ,simulation results show the accuracy of this program.
For a certain type of small unmanned aerial vehicles (SUAV), using the vortex lattice method (VLM) estimated the aerodynamic derivatives, establishing linear small-perturbation equations based on level and non-sideslipping flight. Analyzed the static stability and mode characteristics based on the dimensionless derivative and matlab simulation. Early in the design, by mechanism modeling and performance analysis for the UAV through pneumatic calculations could get a lot of valuable reference data of the UAV. This has some practical significance for system performance analysis and flight control system design.
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