Trajectory tracking and vibration suppression of a 3-PRR parallel manipulator with flexible links

被引:61
作者
Zhang, Quan [1 ,2 ]
Mills, James K. [2 ]
Cleghorn, William L. [2 ]
Jin, Jiamei [1 ]
Zhao, Chunsheng [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Jiangsu, Peoples R China
[2] Univ Toronto, Dept Mech & Ind Engn, Toronto, ON M5S 3G8, Canada
基金
中国国家自然科学基金; 加拿大自然科学与工程研究理事会;
关键词
Flexible parallel manipulator; Dynamic model; Vibration suppression; Singular perturbation; Dual-stage control; HYBRID CONTROL SCHEME; ROBUST TRACKING; ACTIVE CONTROL; FEEDBACK; CONTROLLER; SPACECRAFT; DYNAMICS; DESIGN;
D O I
10.1007/s11044-013-9407-2
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
To achieve high speed, flexible planar parallel manipulators (PPM) are typically designed with lightweight linkages, but hence suffer from unwanted structural vibration, diminishing positioning accuracy. To achieve high positioning accuracy, this paper addresses the vibration suppression of a PPM with three flexible linkages actuated by linear ultrasonic motors (LUSM). Based on the extended Hamilton's principle, a rigid-flexible dynamic model of a proposed PPM is developed using the substructure approach and the assumed mode method (AMM). The assumed mode shapes of the flexible linkages are verified through the experimental modal tests. Then, two control algorithms are designed for tracking control of the end effector and vibration attenuation of the flexible linkages. The first approach is a two-timescale control based on singular perturbation principles, implemented as a joint motion control without additional actuators. The second approach is a dual-stage control method. In this control approach, a variable structural control (VSC) method is applied to realize motion tracking of the moving platform, while the strain and strain rate feedback control (SSRF) is developed to suppress the undesired vibration of the flexible linkages, using multiple distributed collocated lead zirconate titanate (PZT) transducers. Stability analysis of the two algorithms is investigated based on Lyapunov approach. Simulation results of these two approaches show that the dual-stage control method provides better vibration attenuation, and hence, faster settling time of the PPM is achieved.
引用
收藏
页码:27 / 60
页数:34
相关论文
共 44 条
[1]  
[Anonymous], STRUCTURAL DYNAMICS
[2]   PERFORMANCE OF AN ACTIVE CONTROL-SYSTEM WITH PIEZOELECTRIC ACTUATORS [J].
BAZ, A ;
POH, S .
JOURNAL OF SOUND AND VIBRATION, 1988, 126 (02) :327-343
[3]  
Boskovic J.D., 2012, J GUID CONTROL DYNAM, V24, P14
[4]  
deJalon J.G., 1994, KINEMATIC DYNAMIC SI, DOI DOI 10.1007/978-1-4612-2600-0
[5]  
Fahimi F, 2009, AUTONOMOUS ROBOTS: MODELING, PATH PLANNING, AND CONTROL, P1, DOI 10.1007/978-0-387-09538-7
[6]   Active vibration control of flexible steel cantilever beam using piezoelectric actuators [J].
Fei, JT .
Proceedings of the Thirty-Seventh Southeastern Symposium on System Theory, 2005, :35-39
[7]  
Hu Junfeng, 2012, Proceedings of the 2012 Second International Conference on Intelligent System Design and Engineering Application (ISDEA), P744, DOI 10.1109/ISdea.2012.605
[8]   Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics [J].
Hu, Qinglei .
NONLINEAR DYNAMICS, 2008, 52 (03) :227-248
[9]   Robust integral variable structure controller and pulse-width pulse-frequency modulated input shaper design for flexible spacecraft with mismatched uncertainty/disturbance [J].
Hu, Qinglei .
ISA TRANSACTIONS, 2007, 46 (04) :505-518
[10]  
Jalili N., 2009, Piezoelectric-based vibration control: from macro to micro/nano scale systems