Wireless and distributed sensing of the shape of morphing structures

被引:52
作者
Akl, W.
Poh, S.
Baz, A. [1 ]
机构
[1] Univ Maryland, Dept Mech Engn, College Pk, MD 20742 USA
[2] Ain Shams Univ, Dept Design & Prod Engn, Cairo, Egypt
基金
美国国家科学基金会;
关键词
wireless and distributed sensor network; morphing structures; shape monitoring;
D O I
10.1016/j.sna.2007.06.026
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Monitoring the shape of morphing structures is essential for their effective and safe operation. However, current sensing systems such as fiber optic sensors are expensive, brittle, and unsuitable for monitoring large shape changes without being susceptible to failure or performance degradation. Therefore, a new class of sensors that does not suffer from these serious limitations is presented. The sensor system relies in its operation on a specially configured distributed network of wires that is embedded in the composite fabric of these structures. The output of the sensor network is wirelessly transmitted to a control processor to compute the linear and angular deflections, the shape, and maps of the strain distribution over the entire surface of the morphing. The deflection and shape information are vital to ascertain that the structure is properly deployed. The strain map ensures that the structure is not loaded excessively to adversely affecting its service life. The equations governing the operation of the sensor network are developed for a beam-like morphing structure using the non-linear theory of finite elements. The resultin,g equations will provide the sensor with its unique interpolation capabilities that make it possible to map the linear and angular deflection and strain field distribution over the entire surface of the morphing structure. The theoretical and experimental characteristics of the sensor network are determined under static and dynamic loading conditions. The results obtained are used to demonstrate the merits and potential of this new class of sensors as a viable means for monitoring the deflections of 1D morphing structures. Integration of the proposed sensor network with the supporting electronics and with arrays of flexible actuators will enable the development of a self-contained, actively controlled, and autonomously operating new generation of morphing. (C) 2007 Elsevier B.V. All rights reserved.
引用
收藏
页码:94 / 102
页数:9
相关论文
共 12 条
[1]   A new class of distributed sensors [J].
Baz, A ;
Poh, S .
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1997, 119 (04) :582-589
[2]   Modal and physical deflections of beams using distributed wire sensors [J].
Baz, A ;
Poh, S .
SMART MATERIALS & STRUCTURES, 1996, 5 (03) :261-271
[3]   Structural and aeroelastic modeling of general planform wings with morphing airfoils [J].
Gern, FH ;
Inman, DJ ;
Kapania, RK .
AIAA JOURNAL, 2002, 40 (04) :628-637
[4]   Design of a shape-memory alloy actuated macro-scale morphing aircraft mechanism [J].
Manzo, J ;
Garcia, E ;
Wickenheiser, A ;
Horner, GC .
Smart Structures and Materials 2005: Smart Structures and Integrated Systems, 2005, 5764 :232-240
[5]   Biologically-inspired technologies in NASA's Morphing Project [J].
McGowan, AMR ;
Cox, DE ;
Lazos, BS ;
Waszak, MR ;
Raney, DL ;
Siochi, EJ ;
Pao, SP .
SMART STRUCTURES AND MATERIALS 2003: ELECTROACTIVE POLYMER ACTUATORS AND DEVICES (EAPAD), 2003, 5051 :1-13
[6]   Aerodynamic and aeroelastic characteristics of wings with conformal control surfaces for morphing aircraft [J].
Sanders, B ;
Eastep, FE ;
Forster, E .
JOURNAL OF AIRCRAFT, 2003, 40 (01) :94-99
[7]  
Wilson JR, 2002, AEROSPACE AM, V40, P34
[8]   Fiber optic sensors for health monitoring of morphing airframes: I. Bragg grating strain and temperature sensor [J].
Wood, K ;
Brown, T ;
Rogowski, R ;
Jensen, B .
SMART MATERIALS & STRUCTURES, 2000, 9 (02) :163-169
[9]  
[No title captured]
[10]  
[No title captured]