Dynamic model and ADRC of a novel water-air unmanned vehicle for water entry with in-ground effect

被引:16
作者
Qi, Duo [1 ]
Feng, Jinfu [1 ]
Li, Yongli [1 ]
机构
[1] Air Force Engn Univ, Sch Aeronaut & Astronaut Engn, Xian 710038, Peoples R China
关键词
water-air unmanned vehicle; dynamic models; in-ground effect; active disturbance rejection controller (ADRC);
D O I
10.21595/jve.2016.17127
中图分类号
R318 [生物医学工程];
学科分类号
0831 ;
摘要
The class of vehicles that can move both in the air and underwater has been of great interest for decades. A novel water-air unmanned vehicle with double quadrotor structure is designed in this study. The air power mechanism works when the vehicle flies in the air, whereas the water power mechanism works when it moves underwater. The water entry process of water-air unmanned vehicle requires accurate attitude and height control, or the vehicle may bounce off or overturn. However, a force resisting its descent known as in-ground effect will affect its stability. The in-ground effect formula of the water entry process is derived by experiments, and the water entry dynamic model is improved at the same time. An active disturbance rejection controller (ADRC) is designed for the control of water entry attitude and height. Experimental results obtained from the comparison of the ADRC and a proportional-integral-derivative (PID) controller show that the ADRC designed in this study is more robust than the PID controller for the internal coupling and external disturbance on the vehicle. Moreover, the ADRC can meet the requirements of rapid attitude adjustment and accurate height control.
引用
收藏
页码:3743 / 3756
页数:14
相关论文
共 19 条
[1]  
Abhijit D., 2009, J INTELLIGENT ROBOTI, V56, P127
[2]  
[Anonymous], 2007, P AIAA GUIDANCE NAVI
[3]  
[Anonymous], P AIAA GUID NAV CONT
[4]  
Bai Yongqiang, 2012, Robot, V34, P519, DOI 10.3724/SP.J.1218.2012.00519
[5]  
Cheeseman I. C., 1957, TECHNICAL REPORT
[6]  
Han J., 1998, Control and Decision, V13, P19, DOI DOI 10.13195/j.cd.1998.01.19.hanjq.004
[7]  
Hayden J.S., 1976, 32nd annual forum of the American helicopter society, P10
[8]  
Heyson Harry H., 1977, Theoretical study of the effect of ground proximity on the induced e! ciency of helicopter rotors
[9]  
Lee D, 2009, INT J CONTROL AUTOM, V7, P419, DOI [10.1007/s12555-009-0311-8, 10.1007/S12555-009-0311-8]
[10]   Dynamic positioning system based on active disturbance rejection technology [J].
Lei Zhengling ;
Guo Chen ;
Fan Yunsheng .
JOURNAL OF OCEAN UNIVERSITY OF CHINA, 2015, 14 (04) :636-644