-
1
-
-
84992316795
-
Order reduction of aeroelastic models through LK transformation and ricatti iteration
-
August
-
Anderson L.R., Order Reduction of Aeroelastic Models through LK Transformation and Ricatti Iteration, AIAA Paper, AIAA-93-3795-CP, August, 1993, pp. 865-870.
-
(1993)
AIAA Paper, AIAA-93-3795-CP
, pp. 865-870
-
-
Anderson, L.R.1
-
2
-
-
0032208512
-
Applied active control for a nonlinear aeroelastic structure
-
Block J.J., Stragnac T.W., Applied active control for a nonlinear aeroelastic structure, J. Guid. Control Dynam. 21 (6) (1998) 838-845.
-
(1998)
J. Guid. Control Dynam.
, vol.21
, Issue.6
, pp. 838-845
-
-
Block, J.J.1
Stragnac, T.W.2
-
3
-
-
0004252591
-
-
AGARD-R-665, North Atlantic Treaty Organization, Neuilly sur Seine, France, January
-
Breitbach E.J., Effects of Structural Nonlinearities on Aircraft Vibration and Flutter, AGARD-R-665, North Atlantic Treaty Organization, Neuilly sur Seine, France, January, 1978.
-
(1978)
Effects of Structural Nonlinearities on Aircraft Vibration and Flutter
-
-
Breitbach, E.J.1
-
4
-
-
84898490650
-
-
AFFDL-TR-68-161, WPAFB, Dayton, Ohio
-
Burris P.M., Bender M.A., Aircraft Load Alleviation and Mode Stabilization (LAMS) - B52, system analysis, synthesis and design, AFFDL-TR-68-161, WPAFB, Dayton, Ohio, 1968.
-
(1968)
Aircraft Load Alleviation and Mode Stabilization (LAMS) - B52, System Analysis, Synthesis and Design
-
-
Burris, P.M.1
Bender, M.A.2
-
6
-
-
0003823386
-
-
John Wiley & Sons Inc., Toronto
-
Etkin B., Dynamics of Flight, 3rd edition, John Wiley & Sons Inc., Toronto, 1996, pp. 72-74, 120-126, 156-159, 295-299.
-
(1996)
Dynamics of Flight, 3rd Edition
, pp. 72-74
-
-
Etkin, B.1
-
7
-
-
0013479356
-
Transition layers in singular perturbation problems
-
Fife P.C., Transition layers in singular perturbation problems, J. Differ. Equations (1974) 77-105.
-
(1974)
J. Differ. Equations
, pp. 77-105
-
-
Fife, P.C.1
-
9
-
-
0003658323
-
-
Birkhäuser-Verlag, Boston
-
Freemann R.A., Kokotović P.V., Robust Nonlinear Controller Design, Birkhäuser-Verlag, Boston, 1996, pp. 101-136.
-
(1996)
Robust Nonlinear Controller Design
, pp. 101-136
-
-
Freemann, R.A.1
Kokotović, P.V.2
-
10
-
-
85007709933
-
Reduction of stiffness and mass matrices
-
Guyan R.J., Reduction of stiffness and mass matrices, AIAA J. 3 (2) (1965).
-
(1965)
AIAA J.
, vol.3
, Issue.2
-
-
Guyan, R.J.1
-
12
-
-
0025433472
-
Reduced-order aeroelastic models via dynamic residualization
-
Karpel M., Reduced-order aeroelastic models via dynamic residualization, J. Aircraft 27 (1990) 449-455.
-
(1990)
J. Aircraft
, vol.27
, pp. 449-455
-
-
Karpel, M.1
-
13
-
-
0032166295
-
Stability and control of structurally nonlinear aeroelastic system
-
Ko J., Stragnac T.W., Kurdila A.J., Stability and control of structurally nonlinear aeroelastic system, J. Guid. Control Dynam. 21 (5) (1998) 718-725.
-
(1998)
J. Guid. Control Dynam.
, vol.21
, Issue.5
, pp. 718-725
-
-
Ko, J.1
Stragnac, T.W.2
Kurdila, A.J.3
-
15
-
-
84907317855
-
Integral control of large flexible aircraft
-
Ottawa, Canada
-
König K., Schuler J., Integral Control of Large Flexible Aircraft, RTO (AGARD) Symposium, Ottawa, Canada, 1999.
-
(1999)
RTO (AGARD) Symposium
-
-
König, K.1
Schuler, J.2
-
16
-
-
85031470902
-
Robust synergetic design of structural dynamic engine controllers in parameter space
-
to be published
-
Kordt M., Ackermann J., Robust synergetic design of structural dynamic engine controllers in parameter space, J. Guid. Control Dynam. (1999) (to be published).
-
(1999)
J. Guid. Control Dynam.
-
-
Kordt, M.1
Ackermann, J.2
-
17
-
-
0041454430
-
Nonlinear structural controller design applied to flight control actuators
-
Kordt M., Kliffken M.G., Nonlinear structural controller design applied to flight control actuators, Automatisierungstechnik 46 (6) (1998).
-
(1998)
Automatisierungstechnik
, vol.46
, Issue.6
-
-
Kordt, M.1
Kliffken, M.G.2
-
18
-
-
85031469192
-
Parameter robust flight control system for a flexible aircraft
-
Palo Alto, California
-
Kubica F., Livet T., Le Tron X., Bucharels A., Parameter Robust Flight Control System for a Flexible Aircraft, IFAC Automatic Control in Aerospace, Palo Alto, California, 1994.
-
(1994)
IFAC Automatic Control in Aerospace
-
-
Kubica, F.1
Livet, T.2
Le Tron, X.3
Bucharels, A.4
-
19
-
-
0022662802
-
Flutter analysis of a two-dimensional airfoil with cubic nonlinear restoring force
-
National Research Council (Canada) 25438, Ottawa, ON, Canada, February
-
Lee B.H., LeBlanc P., Flutter Analysis of a Two-Dimensional Airfoil with Cubic Nonlinear Restoring Force, National Aeronautical Establishment, Aeronautical Note 36, National Research Council (Canada) 25438, Ottawa, ON, Canada, February, 1986.
-
(1986)
National Aeronautical Establishment, Aeronautical Note 36
-
-
Lee, B.H.1
LeBlanc, P.2
-
20
-
-
0041454479
-
∞ approach to control synthesis with loads minimization for the F/A-18 active aeroelastic wing
-
Hampton, VA, USA
-
∞ Approach to Control Synthesis with Loads Minimization for the F/A-18 Active Aeroelastic Wing, Proceedings of Int. Forum on Aeroelasticity and Structural Dynamics, Hampton, VA, USA, 1999.
-
(1999)
Proceedings of Int. Forum on Aeroelasticity and Structural Dynamics
-
-
Lind, R.1
-
21
-
-
0003426983
-
Robust aeroservoelastic stability analysis
-
Springer-Verlag London, Berlin, Heidelberg
-
Lind R., Brenner M., Robust Aeroservoelastic Stability Analysis, Advances in Industrial Control, Springer-Verlag London, Berlin, Heidelberg, 1999.
-
(1999)
Advances in Industrial Control
-
-
Lind, R.1
Brenner, M.2
-
24
-
-
0004123028
-
Structural loads analysis for commercial transport aircraft: Theory and practice
-
Reston, Virginia
-
Lomax T. D., Structural Loads Analysis for Commercial Transport Aircraft: Theory and Practice, AIAA, Education Series, Reston, Virginia, 1995, pp. 42-45, 143-160.
-
(1995)
AIAA, Education Series
, pp. 42-45
-
-
Lomax, T.D.1
-
25
-
-
0017988807
-
Gust load alleviation control systems for aircraft
-
McLean D., Gust load alleviation control systems for aircraft, P. IEEE. 125 (7) (1978) 675-85.
-
(1978)
P. IEEE.
, vol.125
, Issue.7
, pp. 675-685
-
-
McLean, D.1
-
26
-
-
0003816993
-
-
Prentice Hall International (UK) Ltd., London
-
McLean D., Automatic Flight Control Systems, Prentice Hall International (UK) Ltd., London, 1990, pp. 102-126, 423-429.
-
(1990)
Automatic Flight Control Systems
, pp. 102-126
-
-
McLean, D.1
-
27
-
-
0016071905
-
Optimal inputs for linear system identification
-
Mehra R.K., Optimal inputs for linear system identification, IEEE T. Automat. Contr. AC-19 (3) 1974.
-
(1974)
IEEE T. Automat. Contr.
, vol.AC-19
, Issue.3
-
-
Mehra, R.K.1
-
29
-
-
0004162742
-
-
Springer-Verlag, New York
-
Sepulchre R., Janković M., Kokotović P., Constructive Nonlinear Control, Springer-Verlag, New York, 1997, pp. 276-283.
-
(1997)
Constructive Nonlinear Control
, pp. 276-283
-
-
Sepulchre, R.1
Janković, M.2
Kokotović, P.3
-
30
-
-
0001935145
-
An investigation of effects of certain types of structural nonlinearities on wing and control surface flutter
-
Woolston D.S., Runyan H.L., Andrews R.E., An investigation of effects of certain types of structural nonlinearities on wing and control surface flutter, J. Aeronautical Sci. 24 (1) (1957) 57-63.
-
(1957)
J. Aeronautical Sci.
, vol.24
, Issue.1
, pp. 57-63
-
-
Woolston, D.S.1
Runyan, H.L.2
Andrews, R.E.3
-
31
-
-
0005421803
-
-
Printing and Publication Services Greville House, Cheltenham, Change 14, 27 May
-
Joint Aviation Authority, Joint Aviation Requirements JAR-25 Large Aeroplanes, Printing and Publication Services Greville House, Cheltenham, Change 14, 27 May 1994, pp. 1-C-8.
-
(1994)
Joint Aviation Requirements JAR-25 Large Aeroplanes
-
-
|