Vibration and Aeroelastic Analysis of Highly Flexible HALE Aircraft

[1]  Meyer Nahon,et al.  Mathematical modeling and simulation of a moored buoy system , 1996, OCEANS 96 MTS/IEEE Conference Proceedings. The Coastal Ocean - Prospects for the 21st Century.

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

[3]  Dennis Goege Fast Identification and Characterization of Nonlinearities in Experimental Modal Analysis of Large Aircraft , 2007 .

[4]  D. Peters,et al.  Finite state induced flow models. I - Two-dimensional thin airfoil , 1995 .

[5]  Raymond H. Plaut,et al.  Three-dimensional analysis of submerged, moored, horizontal, rigid cylinders used as breakwaters , 1999 .

[6]  G Kvaternik Raymond,et al.  Exploratory Studies in Generalized Predictive Control for Active Aeroelastic Control of Tiltrotor Aircraft , 2000 .

[7]  G. Vörös,et al.  On the mathematical description of the tensile stress-strain curves of polycrystalline face centered cubic metals , 1996 .

[8]  Roger Bostelman,et al.  The NIST SPIDER, A Robot Crane , 1992, Journal of research of the National Institute of Standards and Technology.

[9]  Fabrizio Vestroni,et al.  Nonlinear oscillations of cables under harmonic loading using analytical and finite element models , 2004 .

[10]  W. H. Reed,et al.  Propeller-Nacelle Whirl Flutter , 1962 .

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

[12]  Mark Drela,et al.  INTEGRATED SIMULATION MODEL FOR PRELIMINARY AERODYNAMIC, STRUCTURAL, AND CONTROL-LAW DESIGN OF AIRCRAFT , 1999 .

[13]  Wei-Jung Shiang,et al.  Dynamic analysis of the cable array robotic crane , 1999, Proceedings 1999 IEEE International Conference on Robotics and Automation (Cat. No.99CH36288C).

[14]  Dennis Göge,et al.  Advanced Test Strategy for Identification and Characterization of Nonlinearities of Aerospace Structures , 2005 .

[15]  J. E. Murray,et al.  Flight testing a highly flexible aircraft - Case study on the MIT Light Eagle , 1990 .

[16]  Alan Shu Khen Kwan,et al.  Shape finding of incomplete cable-strut assemblies containing slack and prestressed elements , 2005 .

[17]  Stanley E. Woodard,et al.  Nonlinear behavior of a passive zero-spring-rate suspension system , 1991 .

[18]  Shan Huang,et al.  Dynamics of small-sagged taut-slack marine cables , 1996 .

[19]  M. Degener,et al.  Modal Identification of Large Aircraft , 1999 .

[20]  Philip S. Beran,et al.  Aeroelastic Analysis of a High-Altitude Long-Endurance Joined-Wing Aircraft , 2005 .

[21]  Jonghoon Park,et al.  Wire-suspended dynamical system: stability analysis by tension-closure , 2005, IEEE Transactions on Robotics.

[22]  Dewey H. Hodges,et al.  Flight Dynamics of Highly Flexible Flying Wings , 2006 .

[23]  Edward F. Crawley,et al.  Very low frequency suspension systems for dynamic testing , 1989 .

[24]  Geoffrey R. Tomlinson,et al.  Use of the Hilbert transform in modal analysis of linear and non-linear structures , 1984 .

[25]  Carlos E. S. Cesnik,et al.  Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft , 2001 .

[26]  N. A. Shul'ga,et al.  Forced Spatial Vibrations of Anchor Cable Systems , 2001 .

[27]  K. A. Blakely Using MSC/NASTRAN to Match Frequency Response Test Data , 1994 .

[28]  P.A.A. Laura,et al.  Analytical and experimental study of the dynamic response of segmented cable systems , 1971 .

[29]  Leonard Meirovitch,et al.  Time Simulations of the Response of Maneuvering Flexible Aircraft , 2003 .

[30]  G. S. Bir Structural Dynamics Verification of Rotorcraft Comprehensive Analysis System (RCAS) , 2005 .

[31]  A. G. James,et al.  Strain energy functions of rubber. I. Characterization of gum vulcanizates , 1975 .

[32]  Dewey H. Hodges,et al.  Analytical and Experimental Study of Beam Torsional Stiffness With Large Axial Elongation , 1988 .

[33]  Dewey H. Hodges,et al.  Geometrically Exact, Intrinsic Theory for Dynamics of Curved and Twisted Anisotropic Beams , 2004 .

[34]  R. Ogden Large Deformation Isotropic Elasticity—On the Correlation of Theory and Experiment for Incompressible Rubberlike Solids , 1973 .

[35]  Leonard Meirovitch,et al.  Unified theory for the dynamics and control of maneuvering flexible aircraft , 2004 .

[36]  Mariella Diaferio,et al.  Smoothed “Slack Cable” Models for Large Amplitude Oscillations of Suspension Bridges , 2004 .

[37]  Marthinus C. Van Schoor,et al.  Aeroelastic characteristics of a highly flexible aircraft , 1990 .

[38]  Lallit Anand,et al.  On H. Hencky’s Approximate Strain-Energy Function for Moderate Deformations , 1979 .

[39]  S. R. Bland,et al.  Experimental and analytical investigation of propeller whirl flutter of a power plant on a flexible wing , 1964 .

[40]  D. Hodges A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams , 1990 .

[41]  Rodney G. Roberts,et al.  On the inverse kinematics, statics, and fault tolerance of cable‐suspended robots , 1998 .

[42]  W. Johnson,et al.  Dynamics of tilting proprotor aircraft in cruise flight , 1974 .

[43]  B. Celikkol,et al.  Numerical modeling of nonlinear elastic components of mooring systems , 2005, IEEE Journal of Oceanic Engineering.

[44]  Inderjit Chopra,et al.  Whirl Flutter Stability of Two-Bladed Proprotor/Pylon Systems In High Speed Flight , 2002 .

[45]  Carlos E. S. Cesnik,et al.  Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow , 2000 .

[46]  Omri Rand,et al.  Experimental demonstration of the influence of wing couplings on Whirl-Flutter instability , 2000 .

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

[48]  Joseph A. Garcia,et al.  A numerical investigation of nonlinear aeroelastic effects on flexible high aspect ratio wings , 2002 .

[49]  Farhan Gandhi,et al.  Active Tiltrotor Whirl-Flutter Stability Augmentation using Wing-Flaperon and Swashplate Actuation , 2005 .

[50]  Sunil K. Agrawal,et al.  Cable suspended robots: design, planning and control , 2002, Proceedings 2002 IEEE International Conference on Robotics and Automation (Cat. No.02CH37292).

[51]  W. Johnson,et al.  Analytical modeling requirements for tilting proprotor aircraft dynamics , 1975 .

[52]  Ronald L. Huston,et al.  Multibody Dynamics Modeling of Variable Length Cable Systems , 2001 .

[53]  Dewey H. Hodges,et al.  Static output feedback control of nonlinear aeroelastic response of a slender wing , 2000 .

[54]  H. K. Edenborough,et al.  Investigation of tilt-rotor VTOL aircraft rotorpylon stability. , 1968 .

[55]  Inderjit Chopra,et al.  Formulation of a Comprehensive Aeroelastic Analysis for Tilt-Rotor Aircraft , 1996 .

[56]  Samuel R. Bland,et al.  An Analytical Treatment of Aircraft Propeller Precession Instability , 1961 .

[57]  Dennis Göge,et al.  Automatic updating of large aircraft models using experimental data from ground vibration testing , 2003 .

[58]  Gaëtan Kerschen,et al.  VTT benchmark: Application of the restoring force surface method , 2003 .

[59]  E. S. Taylor,et al.  Vibration Isolation of Aircraft Power Plants , 1938 .

[60]  Donald L. Kunz,et al.  Analysis of Proprotor Whirl Flutter: Review and Update , 2005 .

[61]  Wei-Jung Shiang,et al.  Optimal force distribution applied to a robotic crane with flexible cables , 2000, Proceedings 2000 ICRA. Millennium Conference. IEEE International Conference on Robotics and Automation. Symposia Proceedings (Cat. No.00CH37065).

[62]  Pao-Hsii Wang,et al.  Study on nonlinear analysis of a highly redundant cable-stayed bridge , 2002 .

[63]  M. Boyce,et al.  A three-dimensional constitutive model for the large stretch behavior of rubber elastic materials , 1993 .

[64]  Jr John E. Teter A Discussion of Zero Spring Rate Mechanisms Used for the Active Isolation Mount Experiment , 1999 .

[65]  R. H. Scanlan The Gyroscopic Effect of a Rigid Rotating Propeller on Engine and Wing Vibration Modes , 1950 .