Limit cycle oscillation prediction using artificial neural networks

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 5, 2001, Pages 887-895

  Denegri C M , Jr ^a   Johnson, M R ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; MULTILAYER NEURAL NETWORKS; OSCILLATIONS;

AEROELASTIC OSCILLATION; LIMIT CYCLE OSCILLATIONS; LINEAR FLUTTER ANALYSIS; NONLINEAR FLUTTER RESPONSE;

FLUTTER (AERODYNAMICS);

EID: 0035441062     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4824     Document Type: Article

References (15)

1. Limit cycle oscillation characteristics of fighter aircraft
2. Limit cycle oscillation and flight flutter testing
3. Semi-empirical unsteady aerodynamics for modeling aircraft limit cycle oscillations and other non-linear aeroelastic problems
4. A semi-empirical unsteady nonlinear aerodynamic model to predict transonic LCO characteristics of fighter aircraft
5. Limit-cycle oscillation studies of a fighter with external stores
6. Evaluation of classical flutter analyses for the prediction of limit cycle oscillations
7. Limit cycle oscillation flight test results of a fighter with external stores
8. An investigation of effects of certain types of structural nonlinearities on wing and control surface flutter
9. Limit cycle oscillations of delta wing models in subsonic flow
10. Limit cycle behavior of an airfoil with a control surface
11. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows
12. An automated procedure for computing flutter eigenvalues
13. Leavenberg-Marquardt method