Full-and reduced- order compensator for innosat attitude control
This paper presents a study on the estimator based on Linear Quadratic Regulator (LQR) control scheme for Innovative Satellite (InnoSAT). By using LQR control scheme, the controller and the estimator has been derived for state space form in all three axes to stabilize the system’s performance. This...
Saved in:
Main Authors: | Siti Maryam, Sharun, Fadzilah, Hashim |
---|---|
Format: | Article |
Language: | English |
Published: |
Penerbit UTM Press
2015
|
Subjects: | |
Online Access: | http://eprints.unisza.edu.my/6725/1/FH02-FSTK-15-04054.jpg http://eprints.unisza.edu.my/6725/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Plug and play innosat ACS simulator
by: Siti Maryam, Sharun, et al.
Published: (2015) -
Internal model control for InnoSAT attitude control
by: M. N, Norhayati, et al.
Published: (2014) -
InnoSAT Attitude Control System Based on Adaptive Neuro-Controller
by: Sharun, Siti Maryam, et al.
Published: (2011) -
Development of attitude control simulator for InnoSAT satellite system
by: Siti Maryam, Sharun, et al.
Published: (2013) -
Attitude Control System for InnoSAT
by: Anon
Published: (2009)