Adaptive Control of Aircraft Wing Oscillations with Stiffness and Damping Nonlinearities in Pitching Mode

Prabhu, L.; Srinivas, J.

doi:10.1007/978-981-10-7563-6_24

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Fluid Control Equation1

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2020

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“…When the physical model studied in this paper is turbulent flow, the corresponding control equation should be added to make the fluid mechanics of the structure closed. Here are the three laws of conservation in physics [17][18][19][20].…”

Section: Fluid Control Equationmentioning

confidence: 99%

Analysis and experimental study on different airfoils in heavy unmanned aerial vehicle

Wang

2020

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The performance of airfoil plays an important role in the performance of model aircraft. Three types of airfoils are selected in this paper: the GOE 480, MH 114, and MH 115, which are all flat-convex airfoils. Firstly, three types of airfoil were numerically analyzed by using Profili software. The results show that among the three types of flat-convex airfoils, the liftdrag ratio of MH series airfoils is higher than that of GOE 480. Then, the FEA software was used to analyze the aerodynamic performance of the wings. And the lift and drag coefficient obtained from calculation was compared with the results by Profili software. To compare the actual flight performance of the three airfoils, the control variable method and UAV self speed measurement method based on sequence images were used for the real field test. The results show that the type of MH 115 has the largest max level speed among the three types of wings.

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Section: Fluid Control Equationmentioning

confidence: 99%

Analysis and experimental study on different airfoils in heavy unmanned aerial vehicle

Wang

2020

View full text Add to dashboard Cite

show abstract

Adaptive Control of Aircraft Wing Oscillations with Stiffness and Damping Nonlinearities in Pitching Mode

Cited by 1 publication

References 14 publications

Analysis and experimental study on different airfoils in heavy unmanned aerial vehicle

Analysis and experimental study on different airfoils in heavy unmanned aerial vehicle

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