Robust Optimization of Aircraft Life-cycle Costs Including the Cost of Community Noise

The paper presents an extension of a formulation for life-cycle-costs-based MDO-CD (Multi-Disciplinary Optimization for Conceptual Design) of aircraft configurations for civil aviation, to take into account the stochastic variation of probabilistic parameters. Specifically, in the formulation used, the community noise is included in the optimization process as a cost. This cost depends a lot, for instance, upon government regulation and community perception, and hence is not necessarily determined when one is performing all the conceptual design computations. Thus, in the formulation presented, the cost of noise is used as a probabilistic design parameter and the optimal design is evaluated as that which minimize the expected value of the aircraft life-cycle-cost. In this preliminary work, the noise produced by the aircraft is evaluated using a simple Noise-Power-Distance model and included in the optimization process. A description of the technique used to estimate the community-noise impact on the life-cycle cost of the aircraft is presented. Applications to the optimization of an aircraft of the A320 category are shown.

[1]  Luigi Morino,et al.  A General Theory of Unsteady Compressible Potential Aerodynamics , 1974 .

[2]  Giovanni Bernardini,et al.  Multidisciplinary Design and Optimization for Fluid-Structure Interactions , 2002 .

[3]  Jaroslaw Sobieszczanski-Sobieski,et al.  OPTIMIZATION OF COUPLED SYSTEMS: A CRITICAL OVERVIEW OF APPROACHES , 1994 .

[4]  Richard J. Balling,et al.  Execution of Multidisciplinary Design Optimization Approaches on Common Test Problems , 1997 .

[5]  Giovanni Bernardini,et al.  Community Noise Considerations in Multidisciplinary Optimization for Preliminary Design of Innovative Configurations , 2004 .

[6]  Giovanni Bernardini,et al.  MDO for Preliminary Design of a Highly Innovative Configuration , 2001 .

[7]  Morris H. DeGroot,et al.  Optimal Statistical Decisions: DeGroot/Statistical Decisions WCL , 2005 .

[8]  Umberto Iemma,et al.  Optimal Conceptual Design of Aircraft Including Community Noise Prediction , 2006 .

[9]  Massimo Gennaretti,et al.  A Velocity Decomposition for Viscous Flows: Lighthill Equivalent-Source Method Revisited , 1997 .

[10]  David E. Goldberg,et al.  Genetic Algorithms in Search Optimization and Machine Learning , 1988 .

[11]  Umberto Iemma,et al.  Community Noise Impact on the Conceptual Design of Innovative Aircraft Configurations , 2005 .

[12]  L. Morino,et al.  Matrix fraction approach for finite-state aerodynamic modeling , 1995 .

[13]  Giovanni Bernardini,et al.  Aerodynamic Issues in MDO for Preliminary Design of an Innovative Configuration , 2002 .

[14]  Umberto Iemma,et al.  Optimal life--cycle--costs design of New Large Aircraft including the cost of community noise , 2005 .

[15]  Igor N. Egorov,et al.  Robust Optimization of Integrated Aircraft-Propulsion System Control to Meet Takeoff Noise Requirements of Supersonic Business Jet , 2004 .

[16]  Giovanni Bernardini,et al.  Life-Cycle Cost Multidisciplinary Optimization for Prandtl-Plane , 2004 .

[17]  Luigi Morino,et al.  Boundary Integral Equations in Aerodynamics , 1993 .