Active flutter control using an adjoint method

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 14, Issue , 2006, Pages 10140-10150

  Palaniappan, Karthik ^a   Sahu, Pradipta ^a   Alonso, Juan ^b   Jameson, Antony ^b  

^a STANFORD UNIVERSITY   (United States)

^b Stanford University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FEEDBACK CONTROL; MATRIX ALGEBRA; NONLINEAR SYSTEMS; PROBLEM SOLVING;

FEEDBACK CONTROL LAW; FLUTTER CONTROL;

FLUTTER (AERODYNAMICS);

EID: 34250731236     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-844     Document Type: Conference Paper

References (5)

1. Raymond L. Bisplinghoff, Holt Ashley, and Robert L. Halfman. Aeroelasticity. Dover Publications, 1996.
2. Antony Jameson. Aerodynamic design via control theory. Journal of Scientific Computing, pages 233-260, 1988.
3. Siva Nadarajah. The Discrete Adjoint Approach to Aerodynamic Shape Optimization. PhD thesis, Stanford University, 2003.
4. T Theodorsen and I. E. Garrick. Mechanism of flutter, a theoretical and experimental investigation of the flutter problem. Technical report, N.A.C.A. Report 685, 1940.
5. Bryson and Ho. Applied Optimal Control: Optimization, Estimation and Control. Taylor and Francis In., 1988.