Satellite Attitude Control Using Hinf Method
碩士 === 國立交通大學 === 電機與控制工程系 === 89 === ABSTRACT The main purpose of this thesis is using method to design the satellite attitude controller,and establish a simple satellite model.We use MATLAB and SIMULINK to do simulation of this controller and analyze,then compare with PD co...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2001
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/89728185617683859355 |
| Summary: | 碩士 === 國立交通大學 === 電機與控制工程系 === 89 === ABSTRACT
The main purpose of this thesis is using method to design the satellite attitude controller,and establish a simple satellite model.We use MATLAB and SIMULINK to do simulation of this controller and analyze,then compare with PD controller.
Simulation results show that under the condition of disturbance,
the auttitude error and angular rate error of controller are 50% to 10% that of PD controller.This show that the controller has good performance and robustness.
|
|---|