Sliding mode control for a dynamic system, helicopter type

Electrical and Electronics Engineering(2013)

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摘要
This paper presents a sliding mode control structure designed for a dynamic system, helicopter type. The approach is robust to model uncertainties and disturbances. The proposed control algorithm is validated on a laboratory stand which uses carrying force to stabilize a helicopter.
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关键词
aircraft control,control system synthesis,helicopters,stability,uncertain systems,variable structure systems,disturbances modeling,dynamic system,helicopter stabilization,helicopter type,robust approach,sliding mode control structure design,uncertainties modeling,control,identification,sliding mode
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