A Fuzzy Theory Based Attitude Control for Takeoff of Quadrotor

被引：0
|
作者：
Yukawa, Chihiro [1 ]
Toyoshima, Kyohei [1 ]
Nagai, Yuki [1 ]
Yamashita, Yuma [3 ]
Saito, Nobuki [2 ]
Oda, Tetsuya [3 ]
Barolli, Leonard [4 ]
机构：
[1] Okayama Univ Sci OUS, Grad Sch Engn, 1-1 Ridaicho,Kita Ku, Okayama 7000005, Japan
[2] Okayama Univ Sci OUS, Grad Sch Sci Engn, 1-1 Ridaicho,Kita Ku, Okayama 7000005, Japan
[3] Okayama Univ Sci OUS, Dept Informat & Comp Engn, 1-1 Ridaicho,Kita Ku, Okayama 7000005, Japan
[4] Fukuoka Inst Technol, Dept Informent & Commun Engn, 3-30-1 Wajiro Higashi Ku, Fukuoka 8110295, Japan
来源：
INNOVATIVE MOBILE AND INTERNET SERVICES IN UBIQUITOUS COMPUTING, IMIS-2023 | 2023年 / 177卷
关键词：
MODEL-PREDICTIVE CONTROL;
D O I：
10.1007/978-3-031-35836-4_6
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
Unmanned Aerial Vehicles (UAVs) are utilized in various fields such as aerial shots, transportation, spraying chemicals in agriculture and surveys of plant growth in forestry. It is necessary to consider the ground effect when operating UAVs/AAVs. The lift coefficient changes and significantly affects the controllability when operating sharp turns within the range of ground effect. So, it is essential to attend to safety-based takeoff and landing as the risk of accidents. In this paper, we propose a fuzzy control for the attitude control of a quadrotor based takeoff.
引用
收藏
页码：47 / 56
页数：10
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