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所属单位：航天学院

发表刊物：AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY

关键字：Sliding mode control Coupling characteristics Unmanned helicopter Hardware in the loop Internal dynamics and external disturbances

摘要：Purpose To facilitate the nonlinear controller design, dynamic model of a novel coaxial unmanned helicopter (UH) is established and its coupling analysis is presented. Design/methodology/approach The chattering-free sliding mode controller (SMC) with unidirectional auxiliary surfaces (UASs) is designed and implemented for the coaxial ducted fan UH. Findings The coupling analysis based on the established model show severe coupling between channels. For coaxial UH's special model structure, UAS-SMC controller is proposed to reduce the coupling characteristics between channels of the UH by setting controllers' output calculation sequence. Originality/value The flight control law and control logic are successfully tested in numerical simulation and hardware in the loop (HIL) simulation. The results show best hovering performances without chattering problem, even under the bounded internal dynamics and external disturbances.

ISSN号：1748-8842

是否译文：否

发表时间：2018-01-01

合写作者：陈挚,甄子洋

通讯作者：陈挚,王道波