Design of Non-linear Dynamic Inversion UAV with QdFT

被引：1
作者：
Li Jie [1 ]
Zhang Jie [2 ]
Xu Zhihui [3 ]
机构：
[1] First Aeronaut Inst AF, Xinyang, Henan, Peoples R China
[2] Weinan Teacher Univ, Training Off, Weinan, Shanxi, Peoples R China
[3] 95168 Unit PLA, Guangzhou, Guangdong, Peoples R China
来源：
INTELLIGENT SYSTEM AND APPLIED MATERIAL, PTS 1 AND 2 | 2012年 / 466-467卷
关键词：
unmanned aerial vehicle(UAV); non-linear dynamic inversion; quantitative feedback theory (QFT); robust;
D O I：
10.4028/www.scientific.net/AMR.466-467.676
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
Flight control system of UAV (Unmanned Aerial Vehicle) has limitations with non-linear dynamic inversion method. This paper introduces QFT based on non-linear dynamic inversion method, for avoiding model errors during existing non-linear function offset, QFT theory is presented firstly, then UAV model is established using non-linear dynamic inversion method, definituding the range of errors and system performance requirements, flight control system of UAV is designed with QFT, the simulating curves show that system has robustness stability.
引用
收藏
页码：676 / +
页数：2
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