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Dynamic Characteristic Analysis of Aerodynamic Load Simulator English
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 Title & Authors
Dynamic Characteristic Analysis of Aerodynamic Load Simulator English
Nam, Yun-Su;
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 Abstract
A dynamic load simulator(DLS) which can reproduce on-ground the aerodynamic hinge moment of control surface is an essential rig for the performance and stability test of aircraft actuation system. By setting up load actuator as counter acting with the control surface driving actuator and designing an appropriate force control system for load actuator, DLS can be mechanized. Obtaining an accurate mathematical model for the DLS is the first step to successfully design an aerodynamic load replicati on system. Two theoretical models are presented and tested for their validities with the experimental results, which turns out to be not successful. An alternative way of using system identification approaches in investigated to develop a good nominal model for DLS dynamics, and suitable uncertainty bounds for this nominal model are proposed with the consideration of experimental results.
 Keywords
Hydraulic Servo Actuator;System Identification;Dynamic Load Simulator;
 Language
Korean
 Cited by
1.
헬리콥터 비행훈련장치용 조종력재현장치의 개발에 관한 연구,한동주;이상행;

대한기계학회논문집A, 2007. vol.31. 10, pp.1031-1038 crossref(new window)
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