Control of Active and Passive Vibration Isolation Stabilization Platform of Airship Based on Characteristic Model

被引:0
作者
Sun Jietao [1 ]
Shen Shaoping [1 ]
Pang Hong [1 ]
机构
[1] Sch Aeronaut & Astronaut, Dept Automat, Xiamen 361005, Peoples R China
来源
PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC) | 2019年
关键词
Active vibration isolation; Stable platform; Characteristic model; Adaptive tracking control; Golden proportional segmentation control; Logical differential control;
D O I
10.23919/chicc.2019.8866308
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
During the flight, the airship load will be subject to various external disturbances, which will make the load camera unclear. To solve this problem, we have established a passive and vibration isolation platform, and used the characteristic model control method in the active vibration isolation system and the stable platform system. Firstly, the super magnetostrictive actuator is selected as the active control component to establish the active-passive integrated vibration isolation platform model. Then the internal relationship of the stable platform is analyzed, and the stepping motor control model of the stable platform is established. Finally, the characteristic modeling is carried out. The identified characteristic parameters are combined with the designed adaptive tracking controller, golden section controller and logic differential controller to control the active vibration isolator and the stable platform. The simulations show that the designed controller is effective.
引用
收藏
页码:2525 / 2530
页数:6
相关论文
共 18 条
[1]  
[Anonymous], ACTA AUTOM SIN
[2]  
Gao Tongyue, 2010, COMPUTER MEASUREMENT, V18
[3]  
Jiheng D, 2018, IEEE-ASME T MECH, P1
[4]  
Karnopp D, 1996, CURRENT ADVANCES IN MECHANICAL DESIGN AND PRODUCTION VI, P409
[5]  
LU Bingzai, 2007, MACHINERY, V45, P24
[6]  
[孟斌 MENG Bin], 2009, [宇航学报, Journal of Chinese Society of Astronautics], V30, P2128
[7]  
Meng Gong, 2012, DESIGN UAV VISUAL ST
[8]   Optimal placement and active vibration control for piezoelectric smart flexible cantilever plate [J].
Qiu, Zhi-Cheng ;
Zhang, Xian-Min ;
Wu, Hong-Xin ;
Zhang, Hong-Hua .
JOURNAL OF SOUND AND VIBRATION, 2007, 301 (3-5) :521-543
[9]  
[王晓磊 Wang Xiaolei], 2005, [宇航学报, Journal of Chinese Society of Astronautics], V26, P275
[10]  
Wu H, 2007, CHARACTERISTIC MODEL