当前位置:
X-MOL 学术
›
J. Aerosp. Eng.
›
论文详情
Our official English website, www.x-mol.net, welcomes your
feedback! (Note: you will need to create a separate account there.)
Enhancing Flight Envelope for a Nonlinear Aeroelastic Wing-Section Using Adaptive Fuzzy Sliding Mode Control Law
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2022-01-27 , DOI: 10.1061/(asce)as.1943-5525.0001401 Smain Dilmi 1
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2022-01-27 , DOI: 10.1061/(asce)as.1943-5525.0001401 Smain Dilmi 1
Affiliation
This paper presents an adaptive fuzzy sliding mode controller (AFSMC) for the control
of a nonlinear aeroelastic wing section. The proposed controller estimates both the
model dynamics of the system and the switching control of the sliding mode. ...
中文翻译:
使用自适应模糊滑模控制律增强非线性气动弹性机翼截面的飞行包络线
本文提出了一种用于控制非线性气动弹性机翼截面的自适应模糊滑模控制器 (AFSMC)。所提出的控制器估计系统的模型动力学和滑模的切换控制。...
更新日期:2022-01-28
中文翻译:
使用自适应模糊滑模控制律增强非线性气动弹性机翼截面的飞行包络线
本文提出了一种用于控制非线性气动弹性机翼截面的自适应模糊滑模控制器 (AFSMC)。所提出的控制器估计系统的模型动力学和滑模的切换控制。...