Modeling the yaw dynamics of an unmanned helicopter through modes partition method

DOI10.1007/S11431-011-4576-9zbMath1421.76142OpenAlexW2056106121MaRDI QIDQ2321227

Hui Xia, GuanLin Wang, XiaMing Yuan, Yong Fan, Ji-Hong Zhu

Publication date: 28 August 2019

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-011-4576-9

zbMATH Keywords

identificationdynamicsgenetic algorithmunmanned helicopter

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Cites Work

• System identification and discrete nonlinear control of miniature helicopters using backstepping
• System identification for a miniature helicopter at hover using fuzzy models
• Identification of linear parameter-varying state-space models with application to helicopter rotor dynamics

This page was built for publication: Modeling the yaw dynamics of an unmanned helicopter through modes partition method