Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/182783
Title: ROBUST CONTROLLER DESIGN FOR A GYRO-MIRROR SYSTEM
Authors: SIEW BOON CHOY
Issue Date: 1997
Citation: SIEW BOON CHOY (1997). ROBUST CONTROLLER DESIGN FOR A GYRO-MIRROR SYSTEM. ScholarBank@NUS Repository.
Abstract: The gyroscope is basically a rotating mass possessing one axis of symmetry and whose rotation about that axis is relatively large compared with the rotation about any other axis. It has two important properties, namely precession and directional stability. Directional stability can be regarded as the reluctance of a body to change its orientation. The target platform of this project - Gyro-stabilized Mirror System, makes use of this property to stabilize its line-of-sight. The gyro-stabilized mirror system is a multivariable servomechanism that is free to rotate about both its yaw and pitch axes. The objective of this project is to design and implement a robust output feedback controller for it. The overall closed-loop system should be able to achieve fast tracking in both axes with smallest possible overshoot. The cross-coupling interaction caused by the precession property of the gyroscope has to be minimized too. The controller design is formulated into the framework of H 00 Almost Disturbance Decoupling Problem with Measurement feedback and internal Stability (H 00-ADDPMS). The results of Chen et al. [23] are then utilized to design a reduced order observer based controller that solves this problem. Simulation and implementation studies show that the overall performance is satisfactory and meets all the design specifications.
URI: https://scholarbank.nus.edu.sg/handle/10635/182783
Appears in Collections:Master's Theses (Restricted)

Show full item record
Files in This Item:
File Description SizeFormatAccess SettingsVersion 
b20648492.pdf4.95 MBAdobe PDF

RESTRICTED

NoneLog In

Google ScholarTM

Check


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.