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Three Axis Stabilization Of Spacecraft Using Parameter Independent Nonlinear Quaternion Feedback by S. M. Joshi
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1NASA Technical Reports Server (NTRS) 19950007316: Three-axis Stabilization Of Spacecraft Using Parameter-independent Nonlinear Quaternion Feedback
By NASA Technical Reports Server (NTRS)
This paper considers the problem of rigid spacecraft. A nonlinear control law which uses the feedback of the unit quaternion and the measured angular velocities is proposed and is shown to provide global asymptotic stability. The control law does not require the knowledge of the system parameters, and is therefore robust to modeling errors. The significance of the control law is that it can be used for large-angle maneuvers with guaranteed stability.
“NASA Technical Reports Server (NTRS) 19950007316: Three-axis Stabilization Of Spacecraft Using Parameter-independent Nonlinear Quaternion Feedback” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19950007316: Three-axis Stabilization Of Spacecraft Using Parameter-independent Nonlinear Quaternion Feedback
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19950007316: Three-axis Stabilization Of Spacecraft Using Parameter-independent Nonlinear Quaternion Feedback” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - ATTITUDE CONTROL - ATTITUDE STABILITY - CONTROL SYSTEMS DESIGN - FEEDBACK CONTROL - NONLINEAR FEEDBACK - QUATERNIONS - SPACECRAFT CONTROL - ANGULAR VELOCITY - NONLINEAR SYSTEMS - Joshi, Suresh M. - Kelkar, Atul G.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19950007316
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The book is available for download in "texts" format, the size of the file-s is: 8.41 Mbs, the file-s for this book were downloaded 77 times, the file-s went public at Fri Oct 07 2016.
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