Dynamics and Control of Flexible Aircraft

[1]  R Waszak Martin,et al.  Modeling and Model Simplification of Aeroelastic Vehicles: An Overview , 1992 .

[2]  Thomas A. Zeiler,et al.  A new simulation model building process for use in dynamic systems integration research , 1987 .

[3]  Peretz P. Friedmann,et al.  Aeroelastic Analysis of a Trimmed Generic Hypersonic Vehicle , 1997, 4th International Symposium on Fluid-Structure Interactions, Aeroelasticity, Flow-Induced Vibration and Noise: Volume III.

[4]  Leonard Meirovitch,et al.  Methods of analytical dynamics , 1970 .

[5]  A Samareh Jamshid,et al.  A Unified Approach to Modeling Multidisciplinary Interactions , 2000 .

[6]  A. S. Taylor The Present Status of Aircraft Stability Problems in the Aeroelastic Domain , 1959 .

[7]  Slobodan R. Sipcic,et al.  Dynamic behavior of fluttering two-dimensional panels on an airplanein pull-up maneuver , 1991 .

[8]  Thomas A. Zeiler,et al.  Nonlinear simulation of a flexible aircraft in maneuvering flight , 1987 .

[9]  T. A. Weisshaar,et al.  Dynamic stability of flexible forward swept wing aircraft , 1983 .

[10]  Klaus H. Well,et al.  Integrated Flight Mechanic and Aeroelastic Modelling and Control of a Flexible Aircraft Considering Multidimensional Gust Input , 2000 .

[11]  L. Meirovitch Principles and techniques of vibrations , 1996 .

[12]  L. Meirovitch,et al.  Derivation of Equations for Flexible Multibody Systems in Terms of Quasi-Coordinates from the Extended Hamilton’s Principle , 1993 .

[13]  David K. Schmidt,et al.  Integrated Development of the Equations of Motion for Elastic Hypersonic Flight Vehicles , 1995 .

[14]  L. Meirovitch,et al.  Hybrid equations of motion for flexible multibody systems using quasicoordinates , 1995 .

[15]  James J. Olsen Unified Flight Mechanics and Aeroelasticity for Accelerating, Maneuvering, Flexible Aircraft , 2000 .

[16]  Klaus Koenig,et al.  Integral Control of Large Flexible Aircraft , 2000 .

[17]  L. Meirovitch,et al.  Structural Modeling for Optimization of Low Aspect Ratio Composite Wings , 1995 .

[18]  Thomas A. Zeiler,et al.  Dynamic analysis of an unrestrained, rotating structure through nonlinear simulation , 1988 .

[19]  John J Cerra Modelling of Rigid-Body and Elastic Aircraft Dynamics for Flight Control Development. , 1986 .

[20]  David K. Schmidt,et al.  Flight dynamics of aeroelastic vehicles , 1988 .

[21]  Martin Goland,et al.  Principles of aeroelasticity , 1975 .

[22]  Leonard Meirovitch,et al.  Dynamics And Control Of Structures , 1990 .

[23]  W. P. Rodden,et al.  Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics , 1985 .

[24]  David K. Schmidt,et al.  Modeling and Simulation of Flexible Flight Vehicles , 2001 .

[25]  K. L. Roger,et al.  Airplane Math Modeling Methods for Active Control Design , 1977 .

[26]  A. R. Collar,et al.  The Expanding Domain of Aeroelasticity , 1946, The Journal of the Royal Aeronautical Society.

[27]  Earl H. Dowell A Modern Course in Aeroelasticity , 1999 .

[28]  H. D. Nelson,et al.  On the high-spin motion of a satellite containing elastic parts. , 1966 .

[29]  J. H. Wykes,et al.  Rigid body-structural mode coupling on a forward swept wing aircraft , 1982 .

[30]  D H Platus,et al.  AEROELASTIC STABILITY OF SLENDER, SPINNING MISSILES , 1989 .

[31]  Leonard Meirovitch,et al.  Hybrid state equations of motion for flexible bodies in terms of quasi-coordinates , 1991 .