A set of fault detection and performance testing system for aircraft flap actuator was introduced, in which the output loading part of the flap actuator was simulated through the hydraulic motor controlling proportional valve. The mathematical modeling and simulation were completed, which could be used as a reference for relevant researches and experiments.
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陈斌,吴惠东,于之靖.襟翼驱动器输出加载系统建模与仿真[J].机床与液压,2017,45(13):143-145. . Modeling and Simulation of the Flaps Actuator Output Loading System[J]. Machine Tool & Hydraulics,2017,45(13):143-145