شماره ركورد كنفرانس :
3296
عنوان مقاله :
Combination of Fault Tolerant Controller and Gyro Bias Observer in Satellite Attitude Determination System
عنوان به زبان ديگر :
Combination of Fault Tolerant Controller and Gyro Bias Observer in Satellite Attitude Determination System
پديدآورندگان :
Nasiri Avanaki Ahmad , Hajatipour Majid Department of Electrical and Computer Engineering University of Kashan - Kashan -Iran , Ahmadian Mohammad Mehdi
كليدواژه :
satellite nonlinear dynamic , gyro bias observer , fault tolerant controller , control subsystem satellite control , attitude determination , component
عنوان كنفرانس :
هجدهمين سمپوزيوم بين المللي علوم كامپيوتر و مهندسي نرم افزار
چكيده لاتين :
in this study, we designed a fault tolerant controller
for satellite attitude determination control system (ADCS) by
combination an adaptive-sliding mode controller and gyro bias
estimator. The observer estimates quaternion and bias error and
then by using satellite kinematics equation, produces real velocity
of satellite. The proposed method could tolerate disturbances in
space and also dynamic uncertainty up to 30% and omit gyro
bias error completely. Stability of combined controller and
observer proved by Lyapunov stability.
