Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table

Momentum changing actuators like reaction wheels and control moment gyros are generally used for spacecraft attitude control. This type of actuators produces force and torque disturbances. These disturbances must be reduced since they degrade the quality of spacecraft attitude control. Major distu...

Full description

Bibliographic Details
Main Authors: Dong-Ik Cheon, Eun-Jeong Jang, Hwa-Suk Oh
Format: Article
Language:English
Published: The Korean Space Science Society 2011-12-01
Series:Journal of Astronomy and Space Sciences
Subjects:
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n4/OJOOBS_2011_v28n4_311.pdf

Similar Items