Longitudinal Fuzzy Model Construction of a Fying-Wing Unmanned Aerial Vehicle and a Nonlinear Guaranteed Cost Control Approach to Altitude Stabilization

被引：0
作者：
Wong, Kai-Yi [1 ]
Kariya, Nana [1 ]
Tanaka, Motoyasu [1 ]
Tanaka, Kazuo [1 ]
机构：
[1] Univ Electrocommun, Dept Mech & Intelligent Syst Engn, Tokyo, Japan
来源：
2019 INTERNATIONAL CONFERENCE ON FUZZY THEORY AND ITS APPLICATIONS (IFUZZY) | 2019年
关键词：
altitude stabilization; guaranteed cost control; longitudinal dynamic model; small flying-wing unmanned aerial vehicle; STABILITY ANALYSIS; SYSTEMS; DESIGN; SUM;
D O I：
暂无
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
This paper presents longitudinal dynamic model construction of a small flying-wing unmanned aerial vehicle (UAV) and a nonlinear control approach to altitude stabilization. The longitudinal dynamic model is constructed by considering its aerodynamics obtained from wind-tunnel experimental results in addition to six-degree-of-freedom dynamics of its body. This paper provides also a fuzzy control approach based on the guaranteed cost control design framework to altitude stabilization. The control approach is compared with the linear LQR design approach. The simulation results demonstrate the utility of our control approach based on the constructed longitudinal dynamic model with the considered aerodynamics.
引用
收藏
页码：151 / 157
页数：7
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