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Author Tafazoli, S. ♦ Khorasani, K.
Sponsorship IEEE Region 10
Source IEEE Xplore Digital Library
Content type Text
Publisher Institute of Electrical and Electronics Engineers, Inc. (IEEE)
File Format PDF
Copyright Year ©2004
Language English
Subject Domain (in DDC) Computer science, information & general works ♦ Data processing & computer science
Subject Keyword Attitude control ♦ Space vehicles ♦ Linear feedback control systems ♦ Nonlinear dynamical systems ♦ Nonlinear equations ♦ Nonlinear control systems ♦ Analytical models ♦ Algorithm design and analysis ♦ Couplings ♦ Coupled mode analysis
Abstract The problem of attitude recovery of flexible spacecraft is investigated using the feedback linearization control approach. The attitude and flexible dynamics equations for a class of spacecrafts are presented. The resulting nonlinear and coupled dynamic equations and the corresponding nonlinear control algorithms of the system are implemented into a high-fidelity, user-friendly simulation environment The simulator is used for both analysis and design investigation of attitude recovery of spacecraft using the feedback linearization approach numerical results for a representative case are included to demonstrate the capabilities of the proposed control and modeling methodologies.
Description Author affiliation: Concordia Univ., Montreal, Que., Canada (Tafazoli, S.; Khorasani, K.)
ISBN 0780385608
Educational Role Student ♦ Teacher
Age Range above 22 year
Educational Use Research ♦ Reading
Education Level UG and PG
Learning Resource Type Article
Publisher Date 2004-11-24
Publisher Place Thailand
Rights Holder Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Size (in Bytes) 1.88 MB
Page Count 4
Starting Page 585
Ending Page 588


Source: IEEE Xplore Digital Library