-
2
-
-
85007688839
-
Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds
-
doi:10.2514/3.43581
-
Zimmerman, N. H., and Weissenburger, J. T., "Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds," Journal of Aircraft, Vol. 1, No. 4, 1964, pp. 190-202. doi:10.2514/3.43581
-
(1964)
Journal of Aircraft
, vol.1
, Issue.4
, pp. 190-202
-
-
Zimmerman, N.H.1
Weissenburger, J.T.2
-
3
-
-
0026896909
-
On-Line Performance Evaluation of Multi-Loop Digital Control Systems
-
July-Aug, doi:10.2514/3.20920
-
Pototzky, A. S., Wieseman, A. S., Hoadley, C. D., and Mukhopadhyay, V., "On-Line Performance Evaluation of Multi-Loop Digital Control Systems," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, July-Aug. 1992, pp. 878-884. doi:10.2514/3.20920
-
(1992)
Journal of Guidance, Control, and Dynamics
, vol.15
, Issue.4
, pp. 878-884
-
-
Pototzky, A.S.1
Wieseman, A.S.2
Hoadley, C.D.3
Mukhopadhyay, V.4
-
4
-
-
0027698616
-
Flight-Determined Multivariable Stability Analysis and Comparison of a Control System
-
doi:10.2514/3.21123
-
Buken, J. J., "Flight-Determined Multivariable Stability Analysis and Comparison of a Control System," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 6, 1993, pp. 1026-1031. doi:10.2514/3.21123
-
(1993)
Journal of Guidance, Control, and Dynamics
, vol.16
, Issue.6
, pp. 1026-1031
-
-
Buken, J.J.1
-
5
-
-
0242273110
-
Flight-Test Evaluation of Flutter Prediction Methods
-
doi:10.2514/2.6881
-
Lind, R., "Flight-Test Evaluation of Flutter Prediction Methods," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 964-970. doi:10.2514/2.6881
-
(2003)
Journal of Aircraft
, vol.40
, Issue.5
, pp. 964-970
-
-
Lind, R.1
-
6
-
-
84910005980
-
Improved Flight Test Procedures for Flutter Clearance," International Forum on Aeroelasticity and Structural Dynamics, Univ. of Rome "La Sapienza
-
June
-
Lind, R., Brenner, M., and Freudinger, L., "Improved Flight Test Procedures for Flutter Clearance," International Forum on Aeroelasticity and Structural Dynamics, Univ. of Rome "La Sapienza," Rome, June 1997, pp. 79-86.
-
(1997)
Rome
, pp. 79-86
-
-
Lind, R.1
Brenner, M.2
Freudinger, L.3
-
7
-
-
29544445182
-
Identifying Parameter-Dependent Volteira Kernels to Predict Aeroelastic Instabilities
-
Nov.-Dec, doi:10.2514/1.12042
-
Lind, R., Prazenica, R. J., Brenner, M. J., and Baldelli, D. H., "Identifying Parameter-Dependent Volteira Kernels to Predict Aeroelastic Instabilities," AIAA Journal, Vol. 43, No. 12, Nov.-Dec. 2005, pp. 2496-2502. doi:10.2514/1.12042
-
(2005)
AIAA Journal
, vol.43
, Issue.12
, pp. 2496-2502
-
-
Lind, R.1
Prazenica, R.J.2
Brenner, M.J.3
Baldelli, D.H.4
-
8
-
-
26244465119
-
Nonlinear Aeroelastic/ Aeroservoelastic Modeling Update by Block-Oriented Identification
-
Sept-Oct, doi:10.2514/1.11792
-
Baldelli, D. H., Lind, R., and Brenner, M., "Nonlinear Aeroelastic/ Aeroservoelastic Modeling Update by Block-Oriented Identification," Journal of Guidance, Control, and Dynamics, Vol. 28, No. 5, Sept-Oct. 2005, pp. 1056-1064. doi:10.2514/1.11792
-
(2005)
Journal of Guidance, Control, and Dynamics
, vol.28
, Issue.5
, pp. 1056-1064
-
-
Baldelli, D.H.1
Lind, R.2
Brenner, M.3
-
9
-
-
84881342938
-
Modeling of Nonlinear System Uncertainties Using a Linear Fractional Transformation Approach
-
Inst. of Electrical and Electronics Engineers, Piscataway, NJ, June
-
Boukarim, G. E., and Chow, J. H., "Modeling of Nonlinear System Uncertainties Using a Linear Fractional Transformation Approach," Proceedings of the American Control Conference, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, June 1998, pp. 2973-2979.
-
(1998)
Proceedings of the American Control Conference
, pp. 2973-2979
-
-
Boukarim, G.E.1
Chow, J.H.2
-
10
-
-
0036178635
-
Match-Point Solutions for Robust Flutter Analysis
-
Jan.-Feb, doi:10.2514/2.290
-
Lind, R., "Match-Point Solutions for Robust Flutter Analysis," Journal of Aircraft, Vol. 39, No. 1, Jan.-Feb. 2002, pp. 91-99. doi:10.2514/2.290
-
(2002)
Journal of Aircraft
, vol.39
, Issue.1
, pp. 91-99
-
-
Lind, R.1
-
11
-
-
51349096662
-
A Poly-Reference Implementation of the Maximum Likelihood Complex Frequency-Domain Estimator and some Industrial Applications
-
Inst. of Electrical and Electronics Engineers, Piscataway, NJ, Jan
-
Cauberghe, B., Guillaume, P., Verboven, P., Parloo, E., and Vanlanduit, S., "A Poly-Reference Implementation of the Maximum Likelihood Complex Frequency-Domain Estimator and some Industrial Applications," 22nd International Modal Analysis Conference, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, Jan. 2004.
-
(2004)
22nd International Modal Analysis Conference
-
-
Cauberghe, B.1
Guillaume, P.2
Verboven, P.3
Parloo, E.4
Vanlanduit, S.5
-
12
-
-
18144402436
-
On the Influence of the Parameter Constraint on the Stability of the Poles and the Discrimination Capabilities of the Stabilization Diagrams
-
doi:10.1016/j.ymssp.2004.07.007
-
Cauberghe, B., Guillaume, P., Verboven, P., Vanlanduit, S., and Parloo, E., "On the Influence of the Parameter Constraint on the Stability of the Poles and the Discrimination Capabilities of the Stabilization Diagrams," Mechanical Systems and Signal Processing, Vol. 19, No. 5, 2005, pp. 989-1014. doi:10.1016/j.ymssp.2004.07.007
-
(2005)
Mechanical Systems and Signal Processing
, vol.19
, Issue.5
, pp. 989-1014
-
-
Cauberghe, B.1
Guillaume, P.2
Verboven, P.3
Vanlanduit, S.4
Parloo, E.5
-
13
-
-
60349131756
-
-
Wahlberg, B., and Olivera e Silva, T., Modelling and Identification with Rational Orthogonal Basis Functions, Springer-Verlag, London, 2005, pp. 15-39.
-
Wahlberg, B., and Olivera e Silva, T., Modelling and Identification with Rational Orthogonal Basis Functions, Springer-Verlag, London, 2005, pp. 15-39.
-
-
-
-
14
-
-
0003426983
-
-
Springer-Verlag, London
-
Lind, R., and Brenner, M., Robust Aeroservoelastic Stability Analysis: Flight Test Applications, Springer-Verlag, London, 1999.
-
(1999)
Robust Aeroservoelastic Stability Analysis: Flight Test Applications
-
-
Lind, R.1
Brenner, M.2
-
15
-
-
0031275376
-
Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity
-
doi:10.2514/2.4174
-
Ko, J., Kurdila, A. J., and Strganac, T. W., "Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1181-1189. doi:10.2514/2.4174
-
(1997)
Journal of Guidance, Control, and Dynamics
, vol.20
, Issue.6
, pp. 1181-1189
-
-
Ko, J.1
Kurdila, A.J.2
Strganac, T.W.3
-
16
-
-
29344463548
-
Aircraft System Identification: Theory and Practice
-
AIAA, Reston, VA
-
Klein, V., and Morelli, E. A., Aircraft System Identification: Theory and Practice, AIAA Education. Series, AIAA, Reston, VA, 2006.
-
(2006)
AIAA Education. Series
-
-
Klein, V.1
Morelli, E.A.2
-
17
-
-
0020879772
-
Flight Test Results of Five Input Signals for Aircraft Parameter Identification
-
Inst. of Electrical and Electronics Engineers, Piscataway, NJ
-
Plaetschke, E., Mulder, J. A., and Breeman, J. H., " Flight Test Results of Five Input Signals for Aircraft Parameter Identification," Proceedings of the Sixth IFAC Symposium on Identification and System Parameter Estimation, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, 1982, pp. 1149-1154.
-
(1982)
Proceedings of the Sixth IFAC Symposium on Identification and System Parameter Estimation
, pp. 1149-1154
-
-
Plaetschke, E.1
Mulder, J.A.2
Breeman, J.H.3
-
18
-
-
33751426587
-
-
AIAA, Reston, VA
-
Jategaonkar, R. V., Flight Vehicle System Identification: A Time Domain Methodology, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2006.
-
(2006)
Flight Vehicle System Identification: A Time Domain Methodology, Progress in Astronautics and Aeronautics
-
-
Jategaonkar, R.V.1
-
19
-
-
0242368081
-
A Flight Test to Demonstrate Flutter and Evaluate the Flutterometer
-
Oct
-
Lind, R., Voracek, D., Truax, R., Doyle, T., Potter, S., and Brenner, M., "A Flight Test to Demonstrate Flutter and Evaluate the Flutterometer," The Aeronautical Journal, Vol. 107, No. 1076, Oct. 2003, pp. 577-588.
-
(2003)
The Aeronautical Journal
, vol.107
, Issue.1076
, pp. 577-588
-
-
Lind, R.1
Voracek, D.2
Truax, R.3
Doyle, T.4
Potter, S.5
Brenner, M.6
|