Type of Document Dissertation Author Newsom, Jerry Russell URN etd-03252002-143535 Title Designing Active Control Laws in a Computational Aeroelasticity Environment Degree PhD Department Mechanical Engineering Advisory Committee

Advisor Name Title Kapania, Rakesh K. Committee Co-Chair Robertshaw, Harry H. Committee Co-Chair Hyer, Michael W. Committee Member Inman, Daniel J. Committee Member Leo, Donald J. Committee Member Keywords

- Active Controls
- Computational Fluid Dynamics
- Aeroelasticity
- Flutter
Date of Defense 2002-04-17 Availability unrestricted AbstractThe purpose of this dissertation is to develop a methodology for designing active control laws in a computational aeroelasticity environment. The methodology involves employing a systems identification technique to develop an explicit state-space model for control law design from the output of a computational aeroelasticity code. The particular computational aeroelasticity code employed in this dissertation solves the transonic small disturbance equation using a time-accurate, finite-difference scheme. Linear structural dynamics equations are integrated simultaneously with the computational fluid dynamics equations to determine the time responses of the structural outputs. These structural outputs are employed as the input to a modern systems identification technique that determines the Markov parameters of an “equivalent linear system”. The eigensystem realization algorithm is then employed to develop an explicit state-space model of the equivalent linear system. Although there are many control law design techniques available, the standard Linear Quadratic Guassian technique is employed in this dissertation. The computational aeroelasticity code is modified to accept control laws and perform closed-loop simulations. Flutter control of a rectangular wing model is chosen to demonstrate the methodology. Various cases are used to illustrate the usefulness of the methodology as the nonlinearity of the computational fluid dynamics system is increased through increased angle-of-attack changes.Files

Filename Size Approximate Download Time (Hours:Minutes:Seconds)

28.8 Modem 56K Modem ISDN (64 Kb) ISDN (128 Kb) Higher-speed Access Dissertation.pdf4.09 Mb 00:18:55 00:09:44 00:08:31 00:04:15 00:00:21

Browse All Available ETDs by
( Author |
Department )

If you have questions or technical problems, please Contact DLA.