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Lateral Stability Analysis For X 29a Drop Model Using System Identification Methodology by David L. Raney
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1NASA Technical Reports Server (NTRS) 19890012431: Lateral Stability Analysis For X-29A Drop Model Using System Identification Methodology
By NASA Technical Reports Server (NTRS)
A 22-percent dynamically scaled replica of the X-29A forward-swept-wing airplane has been flown in radio-controlled drop tests at the NASA Langley Research Center. A system identification study of the recorded data was undertaken to examine the stability and control derivatives that influence the lateral behavior of this vehicle with particular emphasis on an observed wing rock phenomenon. All major lateral stability derivatives and the damping-in-roll derivative were identified for angles of attack from 5 to 80 degrees by using a data-partitioning methodology and a modified stepwise regression algorithm.
“NASA Technical Reports Server (NTRS) 19890012431: Lateral Stability Analysis For X-29A Drop Model Using System Identification Methodology” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19890012431: Lateral Stability Analysis For X-29A Drop Model Using System Identification Methodology
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19890012431: Lateral Stability Analysis For X-29A Drop Model Using System Identification Methodology” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - AIRCRAFT MODELS - DIRECTIONAL STABILITY - DROP TESTS - FLIGHT CHARACTERISTICS - FLIGHT STABILITY TESTS - LATERAL STABILITY - SWEPT FORWARD WINGS - SYSTEM IDENTIFICATION - X-29 AIRCRAFT - AIRCRAFT CONTROL - ANGLE OF ATTACK - REGRESSION ANALYSIS - ROLL - WIND TUNNEL STABILITY TESTS - Raney, David L. - Batterson, James G.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19890012431
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The book is available for download in "texts" format, the size of the file-s is: 23.41 Mbs, the file-s for this book were downloaded 79 times, the file-s went public at Fri Sep 23 2016.
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