Abstract
The design of systems for dynamic response may involve constraints that need to be satisfied over an entire time interval or objective functions evaluated over the interval. Efficiently performing the constrained optimization is challenging, since the typical response is implicitly linked to the design variables through a numerical integration of the governing differential equations. Evaluating constraints is costly, as is the determination of sensitivities to variations in the design variables. In this paper, we investigate the application of a temporal spectral element method to the optimization of transient and time-periodic responses of fundamental engineering systems. Through the spectral discretization, the response is computed globally, thereby enabling a more explicit connection between the response and design variables and facilitating the efficient computation of response sensitivities. Furthermore, the response is captured in a higher order manner to increase analysis accuracy. Two applications of the coupling of dynamic response optimization with the temporal spectral element method are demonstrated. The first application, a one-degree-of-freedom, linear, impact absorber, is selected from the auto industry, and tests the ability of the method to treat transient constraints over a large-time interval. The second application, a related mass-spring-damper system, shows how the method can be used to obtain work and amplitude optimal time-periodic control force subject to constraints over a periodic time interval.
Similar content being viewed by others
References
Afimiwala KA, Mayne RW (1974) Optimum design of an impact absorber. J Eng Ind Trans ASME 96B(1):124–130
Argyris JH, Scharpf DW (1969) Finite elements in time and space. Nucl Eng Des 10(4):456–464
Beran PS, Snyder RD, Blair M (2007) A design optimization strategy for micro air vehicles. AIAA Pap 1853
Burnett DS (1988) Finite element analysis; from concepts to applications. Addison-Wesley, Reading
Choi WS, Park GJ (2002) Structual optimization using equivalent static loads at all time intervals. Comput Methods Appl Mech Eng 191:2077–2094
Etman LFP, Van Campen DH, Schoofs AJG (1998) Design optimization of multibody systems by sequential approximation. Multibody Syst Dyn 2:393–415
Fried I (1969) Finite element analysis of time-dependent phenomena. AIAA J 7:1170–1173
Grandhi RV, Haftka RT, Watson LT (1984) Design oriented identification of critical times in transient response. AIAA Pap 1984–0899
Grandhi RV, Haftka RT, Watson LT (1986) Efficient identification of critical stresses in structures subject to dynamic loads. Comput Struct 22(3):373–386
Haftka RT (1975) Parametric constraints with application to optimization for flutter using a continuous flutter constraint. AIAA J 13(4):471–475
Haftka RT, Gurdal Z (1992) Elements of structural optimization. Kluwer, Dordrecht
Haug EJ, Arora JS (1979) Applied optimal design: mechanical and structural systems. Wiley, New York
Hsieh CC, Arora JS (1984) Design sensitivity analysis and optimization of dynamic response. Appl Math Optim 43(2):195–219
Jameson A (2000) Aerodynamic shape optimization techniques based on control theory. In: Computational mathematics driven by industrial problems (Lecture notes in mathematics), vol 1739. Springer, Heidelberg, pp 151–221
Jameson A, Vassberg JC (2000) Studies of alternative numerical optimization methods applied to the brachistochrone problem. Comput Fluid Dyn 9(3):281–296, October
Kang B-S, Park G-J, Arora JS (2006) A review of optimization of structures subjected to transient loads. Struct Multidisc Optim 31(2):81–95
Kapania RK, Park S (1995) Nonlinear transient response and its sensitivity using finite elements in time. Am Soc Mech Eng Des Eng Div 84(3 Pt B/2):931–942
Karniadakis GE, Sherwin SJ (1999) Spectral/hp element methods for CFD. Oxford University Press, Oxford
Kaya M, Tuncer IH (2007) Path optimization of flapping airfoils based on nurbs. Parallel Comput Fluid Dyn 285–292
Kim NH (2005) Eulerian shape design sensitivity analysis and optimization with a fixed grid. Comput Methods Appl Mech Eng 194(30–33):3291–3314
Kim NH, Choi KK (2001) Design sensitivity analysis and optimization of nonlinear transient dynamics. Mech Struct Mach 29(3):351–371
Klaij CM, van der Vegt JJW, van der Ven H (2006) Space-time discontinuous Galerkin method for the compressible Navier-Stokes equations. J Comput Phys 217(2):589–611
Kurdi MH, Beran PS (2008a) Spectral element method in time for rapidly actuated systems. J Comput Phys 227(3):1809–1835
Kurdi MH, Beran PS (2008b) Optimization of dynamic response using temporal spectral element method. AIAA Pap 0903
Meirovitch L (1986) Elements of vibration analysis. McGraw-Hill, New York
Nadarajah SK, Jameson A (2007) Optimum shape design for unsteady flows with time-accurate continuous and discrete adjoint methods. AIAA J 45(7):1478–1491
Palaniappan K, Beran PS, Jameson A (2006) Optimal control of LCOs in aero-structural systems. AIAA-2006-1621
Park S, Kapania RK, Kim SJ (1999) Nonlinear transient response and second-order sensitivity using time finite element method. AIAA J 37(5):613–622
Patera AT (1984) A spectral element method for fluid dynamics; laminar flow in a channel expansion. J Comput Phys 54:468–488
Pontaza JP, Reddy JN (2004) Space-time coupled spectral/hp least-squares finite element formulation for the incompressible Navier-Stokes equations. J Comput Phys 197(2):418–59
Pozrikidis C (2005) Introduction to finite and spectral element methods using Matlab. Chapman and Hall/CRC, Boca Raton
Raney DL, Slominski EC (2004) Mechanization and control concepts for biologically inspired mirco air vehicles. J Aircraft 41(6):1257–1265
Schutte JF, Koh B-I, Reinbolt JA, Haftka RT, George AD, Fregly BJ (2005) Evaluation of a particle swarm algorithm for biomechanical optimization. J Biomech Eng 127(3):465–74
Shyy W, Berg M, Ljungqvist D (1999) Flapping and flexible wings for biological and micro air vehicles. Prog Aerosp Sci 35(5):455–505
Steidel Jr RF (1989) An introduction to mechanical vibrations. Wiley, New York
van Keulen F, Haftka RT, Kim NH (2005) Review of options for structural design sensitivity analysis. part 1: linear systems. Comput Methods Appl Mech Eng 194(30–33):3213–3243
Venkayya VB, Khot NS, Tischler VA, Taylor RF (1971) Design of optimum structures for dynamic loads. In: The 3rd conference on matrix methods of structural mechanics flight dynamics laboratory, Wright Patterson Air Force Base, Dayton, Ohio, October 1971, pp 619–658
Wilmert KD, Fox RL (1972) Optimum design of a linear multidegree-of-freedom shock isolation system. J Eng Ind 94:465–471
Author information
Authors and Affiliations
Corresponding author
Additional information
This research was performed while the first author held a National Research Council Research Associateship Award at the Air Force Research Laboratory.
An early version of this paper was presented at the 46th AIAA Aerospace Sciences Meeting and Exhibit, Jan 7–10, 2008, Reno, Nevada.
Rights and permissions
About this article
Cite this article
Kurdi, M.H., Beran, P.S. Optimization of dynamic response using a monolithic-time formulation. Struct Multidisc Optim 39, 83–104 (2009). https://doi.org/10.1007/s00158-008-0316-6
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s00158-008-0316-6