Torque Mode-Based Flywheel System For Small Satellite Attitude Control
One of the most important problems in satellite design is that of attitude control. An architecture of attitude control for small satellite using flywheel system is proposed. This flywheel system can combinedly perform both the energy and attitude control task that are the crucial area for all ty...
Saved in:
Main Author: | Mehedi, Ibrahim Mustapa |
---|---|
Format: | Thesis |
Language: | English |
Published: |
2005
|
Subjects: | |
Online Access: | http://psasir.upm.edu.my/id/eprint/6064/1/FK_2005_50.pdf http://psasir.upm.edu.my/id/eprint/6064/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Design and simulation of a hybrid flywheel bus
by: Masoud Masih Tehrani, et al.
Published: (2012) -
Development of an adaptive neurocontroller and satellite simulator for nano-satellite attitude control system
by: Siti Maryam, Sharun
Published: (2014) -
Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
by: Muhamad Asraf, Basharudin
Published: (2016) -
Adaptive neuro-controller design for nano-satellite attitude control
by: Norhayati, Mohd Nazid
Published: (2014) -
Adaptive Neuro-Controller for three axes attitude control of innovative satellite
by: Siti Maryam Sharun, et al.
Published: (2011)