Fuzzy Adaptive Attitude Controller Design for Launch Vehicle

被引：0
|
作者：
Pei, Wang [1 ]
Bo, Lv Mei [1 ]
Lei, Ge Zhi [1 ]
Shan, Xu [1 ]
机构：
[1] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, Coll Astronaut, Xian, Shaanxi, Peoples R China
来源：
2017 INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION SCIENCES (ICRAS) | 2017年
关键词：
launch vehicle; attitude control; fuzzy logic system; proportional-differential control;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Launch vehicle attitude control is a complex nonlinear problem that is compounded by several internal and external factors such as modeling uncertainties, fuel sloshing and unstable aerodynamics. An anti-interference attitude controller of launch vehicle based on fuzzy logic system (FLS) and proportional-differential (PD) control is proposed to attenuate the effect of parameter variation and disturbances on attitude control accuracy and stability. The FLS is designed to estimate and compensate impact of parametric uncertainties and disturbances, when used in conjunction with a proportional derivative (PD) controller offers improved the attitude control performance when encountering uncertainty and external disturbances. Further, the comparison simulation of the FLS augmented PD controller with a traditional PD controller is done. The results show that the controller exhibits better dynamic performance, stronger robustness.
引用
收藏
页码：58 / 63
页数：6
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