DocumentCode
539628
Title
Control System Design and Simulation of an Aerial Three-Axis ISP System Based on SimMechanics
Author
Jianping, Li ; Xiangyang, Zhou ; Quanqi, Mu ; Du Lei
Author_Institution
Sch. of Instrum. Sci. & Opto-Electron. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Volume
1
fYear
2011
fDate
6-7 Jan. 2011
Firstpage
778
Lastpage
781
Abstract
The main purpose of this paper is to investigate the control method for a three-axis ISP. Firstly, a simplified geometry model was built by Solid works. Then, a Simulink model composed of bodies, joints, constraints, and force elements of ISP was obtained from the 3D model via SimMechanic toolbox. On the basis of the Simulink model, the classical PID controllers and three closed servo loops were designed and applied to the ISP system under the friction disturbance being taken into account. The simulation results show that compared to the roll and pitch gimbals, the dynamic performance of the yaw gimbal is severely affected by the friction and whose proportion in position loop needs to be adjusted if a better dynamic performance is got.
Keywords
aerospace instrumentation; closed loop systems; control engineering computing; inertial systems; servomechanisms; solid modelling; three-term control; PID controllers; SimMechanics; Simulink model; Solidworks; aerial three axis ISP system; closed servo loops; control system design; geometry model; pitch gimbals; roll gimbals; yaw gimbal; Friction; Image sensors; Interference; Remote sensing; Servomotors; Solid modeling; PID; Servo Control; SimMechanic; Three-Axis ISP;
fLanguage
English
Publisher
ieee
Conference_Titel
Measuring Technology and Mechatronics Automation (ICMTMA), 2011 Third International Conference on
Conference_Location
Shangshai
Print_ISBN
978-1-4244-9010-3
Type
conf
DOI
10.1109/ICMTMA.2011.196
Filename
5720899
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