Active vibration isolation using a six-axis orthogonal vibration isolation platform with piezoelectric actuators

被引:7
作者
Wang, Shuai [1 ]
Chen, Zhaobo [1 ]
Jiao, Yinghou [1 ]
Liu, Xiaoxiang [2 ]
机构
[1] Harbin Inst Technol, Sch Mechatron Engn, Harbin, Heilongjiang, Peoples R China
[2] Beijing Inst Control Engn, 16 South 3rd St, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
piezoelectric actuators; vibration isolation platform; decoupling control; LQR; SYSTEM; SPACE;
D O I
10.21595/jve.2017.19014
中图分类号
R318 [生物医学工程];
学科分类号
0831 ;
摘要
Piezoelectric actuators (PEA) act an important role in active vibration control area due to the advantages of fast response, high output force, small size and light weight. A 6-axis orthogonal vibration isolation platform based on PEAs is designed, which satisfies the demands of heavy payload, small installation space and multi degree of freedom vibration isolation. The dynamic model of the six-axis orthogonal vibration isolation platform with PEAs is established using Newton-Euler method. With the layout of six PEAs around the axis of symmetry, the dynamic equations could be decoupled into two single-input-single-output (SISO) subsystems and two multi-input-multi-output (MIMO) subsystems. Based on the modal superposition method, the two MIMO subsystems are further decoupled. The control strategy for each SISO system is developed with LQR control method. To evaluate the effectiveness of the control method, the simulation and verification experiment are conducted. The simulation result and experimental data indicate that the decoupling control of the proposed six-axis orthogonal vibration isolation platform with piezoelectric actuators effectively reduces the vibration response of payload within the target frequency range of 20 Hz to 200 Hz.
引用
收藏
页码:6105 / 6121
页数:17
相关论文
共 28 条
[1]  
Abu Hanieh A, 2001, ESA SP PUBL, V480, P331
[2]  
Abu Hanieh A., 2003, ACTIVE ISOLATION DAM
[3]  
Anderson E. H., 1999, AEROSPACE C P IEEE, V4, P299
[4]  
Argentim L.M., 2013, 2013 INT C INFORMATI, P1
[5]   MLCD: Overview of NASA's mars laser communications demonstration system [J].
Boroson, DM ;
Biswas, A ;
Edwards, BL .
FREE-SPACE LASER COMMUNICATION TECHNOLOGIES XVI, 2004, 5338 :16-28
[6]   Vibration isolator for large space telescopes [J].
Bronowicki, AJ .
JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (01) :45-53
[7]   Decoupled control of flexure-jointed hexapods using estimated joint-space mass-inertia matrix [J].
Chen, YX ;
McInroy, JE .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2004, 12 (03) :413-421
[8]   Vibration isolation and suppression system for precision payloads in space [J].
Cobb, RG ;
Sullivan, JM ;
Das, A ;
Davis, LP ;
Hyde, TT ;
Davis, T ;
Rahman, ZH ;
Spanos, JT .
SMART MATERIALS & STRUCTURES, 1999, 8 (06) :798-812
[9]  
Davis L.P., 2013, 35 STRUCT STRUCT DYN, V32, P43
[10]  
Ford V., 2005, P INT ASTRONOMICAL U, V1, P335