Show simple item record

dc.contributor.authorLi, Xianying
dc.contributor.authorZhao, Biao
dc.contributor.authorYao, Yu
dc.contributor.authorWu, Hongtao
dc.contributor.authorLiu, Yunping
dc.date.accessioned2019-02-28T11:11:52Z
dc.date.available2019-02-28T11:11:52Z
dc.date.copyright1/10/2018 12:00:00 AM
dc.date.issued2018
dc.identifier.issn1555-1415
dc.identifier.othercnd_013_03_031005.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253720
dc.description.abstractThe effect of wind disturbances on the stability of six-rotor unmanned aerial vehicles (UAVs) was investigated, exploring the various disturbances in different directions. The simulation model-based Euler–Poincare equation was established to investigate the spectra of Lyapunov exponents. Next, the value of the Lyapunov exponents was used to evaluate the stability of the systems. The results obtained show that the various speeds of rotors are optimized to keep up the stability after disturbances. In addition, the flight experiment with the hitting gust has been carried out to verify the validity and accuracy of the simulation results.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleStability and Performance Analysis of Six-Rotor Unmanned Aerial Vehicles in Wind Disturbance
dc.typeJournal Paper
dc.journal.volume13
dc.journal.issue3
dc.journal.titleJournal of Computational and Nonlinear Dynamics
dc.identifier.doi10.1115/1.4038776
dc.journal.fristpage31005
dc.journal.lastpage031005-11
dc.treeJournal of Computational and Nonlinear Dynamics:;2018:;volume( 013 ):;issue: 003
dc.contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record