A probabilistic hybrid sensor fusion and optimization approach for aircraft composite components

An integrated sensor system that continuously monitors the structural integrity of an aircraft’s critical composite components can have a high payoff by reducing risks, costs, inspections, and unscheduled maintenance, while increasing safety. Hybrid sensor networks combine or fuse different types of sensors. Optimal sensor fusion tries to find the optimal number and location of different types of sensors such that their combined probability of detection is maximized. Optimal hybrid sensor networks can be more robust, more accurate, and/or cheaper than networks consisting only of homogeneous sensors. A generic sensor fusion approach that combines the probabilities of detection of heterogeneous sensors is described. A fast greedy optimization approach that provides approximate solutions is described and demonstrated. Computable lower and upper bounds of a probability of detection objective function were determined. Fiber Bragg grating sensors can be inserted in layers of composite structures to provide local damage detection, while surface-mounted piezoelectric lead zirconate titanate sensors can provide global damage detection for the host structure under consideration. The generic approach is demonstrated on such combinations of fiber Bragg grating and lead zirconate titanate sensor networks. It is demonstrated that the proposed approach can be used to answer structural health monitoring network design problems such as the following: (1) Given a number of sensors, what is the maximum probability of detection that the sensors can attain and where should they be positioned to provide the maximum probability of detection? (2) If a given probability of detection is desired, the minimum number, types, and locations of sensors that are needed to attain this probability of detection can be determined. The approach is generic, that is, it can be extended to any number or types of sensors for which probabilities of detection can be defined.

[1]  Bordick,et al.  Analysis of Interlaminar Damages in Thick Rotorcraft Composite Components by Embedded Sensors , 2010 .

[2]  Anindya Ghoshal,et al.  Development of Embedded Sensor Models in Composite Laminates for Structural Health Monitoring , 2004 .

[3]  L Padula Sharon,et al.  Optimization Strategies for Sensor and Actuator Placement , 1999 .

[4]  Anindya Ghoshal,et al.  Development of embedded piezoelectric acoustic sensor array architecture , 2010, Microelectron. Reliab..

[5]  Hui Li,et al.  Application of information fusion and Shannon entropy in structural damage detection , 2007, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[6]  Eric B. Flynn,et al.  Bayesian probabilistic structural modeling for optimal sensor placement in ultrasonic guided wave-based structural health monitoring , 2010, Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[7]  Hyun-Kyu Kang,et al.  Detection of Buckling and Crack Growth in the Delaminated Composites Using Fiber Optic Sensor , 2000 .

[8]  Anindya Ghoshal,et al.  Effect of embedded sensors on interlaminar damage in composite structures , 2011 .

[9]  Jeong-Beom Ihn,et al.  A Potential Link from Damage Diagnostics to Health Prognostics of Composites through Built-in Sensors , 2007 .

[10]  Xiaohong Yuan,et al.  Engine fault diagnosis based on multi-sensor information fusion using Dempster-Shafer evidence theory , 2007, Inf. Fusion.

[11]  J. Michaels,et al.  Feature Extraction and Sensor Fusion for Ultrasonic Structural Health Monitoring Under Changing Environmental Conditions , 2009, IEEE Sensors Journal.

[12]  Gary L. Anderson,et al.  Current and potential future research activities in adaptive structures: an ARO perspective , 2001 .

[13]  J. Pintér Global optimization : scientific and engineering case studies , 2006 .

[14]  Anindya Ghoshal,et al.  Ultrasonic Simulation of Interlaminar Damages in Rotorcraft Composite Components: Approach and Parametric Analysis , 2011 .

[15]  D. Inman,et al.  Health monitoring and active control of composite structures using piezoceramic patches , 1999 .

[16]  Victor Giurgiutiu,et al.  Finite element simulation of piezoelectric wafer active sensors for structural health monitoring with coupled-filed elements , 2007, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[17]  Eric B. Flynn,et al.  A Bayesian approach to optimal sensor placement for structural health monitoring with application to active sensing , 2010 .

[18]  A. J. Booker,et al.  A rigorous framework for optimization of expensive functions by surrogates , 1998 .

[19]  Anindya Ghoshal,et al.  Smart Embedded Sensors in Rotorcraft Composite Components for Condition Based Maintenance , 2010 .

[20]  M. Morelli,et al.  Application of Dempster-Shafer theory of evidence to the correlation problem , 2002, Proceedings of the Fifth International Conference on Information Fusion. FUSION 2002. (IEEE Cat.No.02EX5997).

[21]  P. Pardalos,et al.  Handbook of global optimization , 1995 .

[22]  Antonia Papandreou-Suppappola,et al.  Sensor optimization for progressive damage diagnosis in complex structures , 2010, Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[23]  Antonia Papandreou-Suppappola,et al.  Structural damage detection with insufficient data using transfer learning techniques , 2011, Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[24]  Anindya Ghoshal,et al.  Damage Detection Testing on a Helicopter Flexbeam , 2001 .

[25]  G. Meltz,et al.  Formation of Bragg gratings in optical fibers by a transverse holographic method. , 1989, Optics letters.

[26]  Aditi Chattopadhyay,et al.  Optimization of piezoelectric sensor location for delamination detection in composite laminates , 2006 .

[27]  Anindya Ghoshal,et al.  Optimal FBG Sensor Placement in Composite Components: Algorithm and Sensor Type Trade Studies , 2011 .

[28]  Hiroshi Asanuma,et al.  Proposal of an active composite with embedded sensor , 2002 .

[29]  C. Floudas Nonlinear and Mixed-Integer Optimization: Fundamentals and Applications , 1995 .

[30]  W. Staszewski,et al.  Sensor location studies for damage detection with Lamb waves , 2007 .

[31]  W. Staszewski,et al.  Impact damage location in composite structures using optimized sensor triangulation procedure , 2003 .

[32]  Bo-Suk Yang,et al.  Application of Dempster–Shafer theory in fault diagnosis of induction motors using vibration and current signals , 2006 .

[33]  A. Baker,et al.  Composite Materials for Aircraft Structures , 2004 .

[34]  S. Chang,et al.  Heat Transfer in a Radially Rotating Square-Sectioned Duct With Two Opposite Walls Roughened by 45Deg Staggered Ribs at High Rotation Numbers , 2007 .