IEEE - Institute of Electrical and Electronics Engineers, Inc. - Comment on “Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults”

Author(s): Seyed Majid Esmailzadeh ; Mehdi Golestani
Sponsor(s): IEEE Control Systems Society
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 July 2019
Volume: 27
Page(s): 1,846
ISSN (CD): 2374-0159
ISSN (Electronic): 1558-0865
ISSN (Paper): 1063-6536
DOI: 10.1109/TCST.2018.2804921
Regular:

Based on a new fixed-time sliding mode control, a finite-time control for attitude stabilization of a rigid spacecraft subject to external disturbance, actuator faults, and input saturation has... View More

Advertisement