Static shape control for adaptive wings

AIAA Journal

Volumn 32, Issue 9, 1994, Pages 1895-1901

  Austin, Fred ^a   Rossi, Michael J ^a   Nostrand, William Van ^a   Knowles, Gareth ^a   Jameson, Antony ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b PRINCETON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CONTROL SYSTEMS; DEFORMATION; DRAG; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; LOADS (FORCES); MATHEMATICAL MODELS; MATRIX ALGEBRA; MODIFICATION; STRUCTURAL ANALYSIS; WINGS;

ACTUATOR DISPLACEMENT CONTROL; ACTUATOR LOAD CONTROL; ADAPTIVE WING; CONTROLLED STRUCTURE THEORY; GAIN MATRIES; MULTIPLE INPUT MULTIPLE OUTPUT CONTROL SYSTEM; SHOCK INDUCED DRAG; STATIC SHAPE CONTROL; TRANSONIC CRUISE FLIGHT CONDITIONS;

FLEXIBLE STRUCTURES;

ADAPTIVE; MODELLING-MATHEMATICAL; SHAPE; STATIC CONTROL; WINGS;

EID: 0028501727     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.12189     Document Type: Article

References (9)

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2. Spillman, J. J., “The Use of Variable Camber to Reduce Drag, Weight and Costs of Transport Aircraft,” Aeronautical Journal, Vol. 96, No. 951, 1992, pp. 1-9.
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8. Jameson, A., “Automatic Design of Transonic Airfoils to Reduce Shock Induced Pressure Drag,” Princeton Univ. Rept. MAE 1881, Princeton, NJ, Feb. 1990
9. Jameson, A., Proceedings of the 31st Israel Annual Conference on Aviation and Aeronautics (Tel Aviv), Technion, Haifa, Israel, 1990, pp. 5-17.