2017 Vol. 43, No. 8

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Health state prediction technique for aircraft wing based on MEMD and ELM
CUI Jianguo, XU Lingyu, YU Mingyue, JIANG Liying, WANG Jinglin, LIN Zeli
2017, 43(8): 1501-1508. doi: 10.13700/j.bh.1001-5965.2016.0610
Abstract:

Composite materials are more and more widely used in the modern aircraft structure. In order to effectively forecast the health state of aircraft wing, the multivariate empirical mode decomposition (MEMD) energy entropy and extreme learning machine (ELM) model are introduced into prediction method o...

Localization and imaging of crack damage in plate-like structures based on vibro-acousic modulation
YANG Xiaohua, LIU Xuejun, ZHANG Ding, XIN Zhidong
2017, 43(8): 1509-1516. doi: 10.13700/j.bh.1001-5965.2016.0595
Abstract:

To overcome the shortcomings of linear Lamb waves in closed crack and micro crack monitoring, a imaging method of crack damage localization in plate-like structure based on vibro-acoustic modulation theory and delay and sum algorithm is proposed. The signal components of acoustic wave are analyzed i...

Propagation characteristics of photonic bandgap fiber collimator with C-lens
LI Yan, ZHAO Yuan, XU Xiaobin, CAI Wei
2017, 43(8): 1517-1522. doi: 10.13700/j.bh.1001-5965.2016.0581
Abstract:

A photonic bandgap fiber collimator with C-lens was proposed. The photonic crystal fiber end face does not have reflection, so the transform matrix will change. From the general model of Gaussian-beam imaging, using the theory of matrix optics, the matrix optics was calculated in meridian plane and ...

Research on performance of variable geometry turbocharger for aero engine
XU Bin, ZHOU Fan, YANG Shichun, TIAN Fugang, TAN Longxing
2017, 43(8): 1523-1530. doi: 10.13700/j.bh.1001-5965.2016.0639
Abstract:

A variable geometry turbocharger method was used to adjust the power of the engine. It's regulation law and characteristics was studied. According to the turbine flow model, the influence of different nozzle ring opening degrees on the turbocharger was analyzed under the same operating conditions. I...

Regenerative brake strategy based on braking boundary and intention recognition
WU Zhixin, SHI Jinpeng, LI Yalun, YANG Haisheng, MA Shaodong
2017, 43(8): 1531-1540. doi: 10.13700/j.bh.1001-5965.2016.0645
Abstract:

Effective strategy of regenerative brake can increase the recycling energy and improve the driving range of electric vehicles. A recycling brake force distribution strategy on the basis of maximum boundary was proposed from the analysis of the vehicle brake dynamics and related regulations. The mode...

Design and comparative analysis of flight trajectory of airborne earth observation
GONG Xiaolin, ZHANG Shuai
2017, 43(8): 1541-1549. doi: 10.13700/j.bh.1001-5965.2016.0580
Abstract:

Aimed at the problem of attitude errors of distributed position and orientation system (POS) accumulate over time when airborne earth observation aircraft moves along a straight line at a constant velocity, a variety of maneuver modes were designed. Not only the estimation accuracy of distributed PO...

Performance optimization for 150 kV inverter power supply and its electron beam source characteristics
XU Haiying, SANG Xinghua, ZHANG Wei, QI Bojin
2017, 43(8): 1550-1558. doi: 10.13700/j.bh.1001-5965.2016.0651
Abstract:

In order to enhance the stability and reliability of electron beam source system and improve the machining quality of electron beam, the topology circuit of AC-DC-AC-DC-AC-DC, new power transformer, high voltage pulse detection technology, optimized feedback control technology of electron beam and c...

Influence of continuous trailing-edge variable camber wing on aerodynamic characteristics of airliner
GUO Tongbiao, BAI Junqiang, YANG Yixiong
2017, 43(8): 1559-1566. doi: 10.13700/j.bh.1001-5965.2016.0583
Abstract:

The continuous trailing-edge variable camber wing has a potential in improving the aerodynamic characteristics of the airliner, and is widely concerned recently. Based on the optimization design system constructed in this paper, the influence of continuous trailing-edge variable camber wing on the a...

Numerical analysis of pitching moment non-linear characteristics of diamond joined-wing configuration
SUN Junlei, WANG Heping, ZHOU Zhou, WANG Ziyi
2017, 43(8): 1567-1576. doi: 10.13700/j.bh.1001-5965.2016.0584
Abstract:

Investigation on the pitching moment non-linear characteristics of the high-attitude long-endurance (HALE) diamond joined-wing configuration unmanned aerial vehicle (UAV) was carried out by both numerical simulation and theoretical analysis method. The results show that the aircraft have two obvious...

A modified weighted round robin scheduling algorithm in TTE
ZHANG Yingjing, HE Feng, LU Guangshan, XIONG Huagang
2017, 43(8): 1577-1584. doi: 10.13700/j.bh.1001-5965.2016.0590
Abstract:

TT messages that have the top priority among three kinds of traffics affect RC message communication inevitably in time-triggered Ethernet (TTE). Therefore, RC messages have to be scheduled among discrete time slices caused by TT message offline schedule table. A modified weighted round robin (MWRR)...

Performance of delayed functions in DDES for supersonic base flow
DU Ruofan, YAN Chao, HAN Zheng, XIANG Xinghao, QU Feng
2017, 43(8): 1585-1593. doi: 10.13700/j.bh.1001-5965.2016.0602
Abstract:

The DDES is a widely used approach among RANS/LES hybrid methods. It introduces the delayed function to ensure full RANS mode in the near-wall region, and has been proven to be quite efficient for separated flows. Up to date, various different delayed functions have been developed. However, the unde...

Design of guidance law with multiple constraints considering maneuvering efficiency
WANG Chaolun, XUE Lin, YAN Xiaoyong
2017, 43(8): 1594-1601. doi: 10.13700/j.bh.1001-5965.2016.0567
Abstract:

Due to the guidance law with terminal intercept angle which will cause big angle error when available payload is insufficient, a guidance law considering time-varying overload constraint has been elicited, which would bring on more energy loss when much maneuver is achieved at the same time. Given t...

Compact shock capturing scheme for compressible multiscale flow
LI Yansu, YAN Chao, YU Jian
2017, 43(8): 1602-1609. doi: 10.13700/j.bh.1001-5965.2016.0623
Abstract:

Aimed at compressible multiscale flow simulations, a fifth-order high-resolution compact shock capturing scheme, compact-reconstruction weighted essentially non-oscillatory (CRWENO), is studied. Nonlinear weights are used to combine lower-order compact schemes to approximate a higher-order compact s...

GNSS sea surface reflection signal modeling method based on principle of bistatic radar
QI Yongqiang, ZHANG Bo, YANG Dongkai, ZHANG Yanzhong, WANG Qiang
2017, 43(8): 1610-1615. doi: 10.13700/j.bh.1001-5965.2016.0631
Abstract:

In the application of global navigation satellite system-reflection(GNSS-R) technology, the reflection signal source is needed to test the receiver in order to reduce costs. The signal model is the core of GNSS-R signal source. In order to solve the problem of the lack of corresponding model, this p...

Optimization strategy of supercritical laminar flow airfoil design
XING Yu, LUO Dongming, YU Xiongqing
2017, 43(8): 1616-1624. doi: 10.13700/j.bh.1001-5965.2016.0656
Abstract:

A two-step optimization strategy for the supercritical laminar flow airfoil design is proposed in the paper. The γ-Reθt transition model coupled with the shear stress transportation (SST) turbulence model is used for prediction of airfoil boundary layer transition. The Class/Shape Transformation (CS...

Modeling and analysis of spares supply support relations among three stations
ZHANG Ying, WANG Yun, XUE Pei
2017, 43(8): 1625-1631. doi: 10.13700/j.bh.1001-5965.2016.0709
Abstract:

For modeling, the existing spares-related researches have insufficient consideration of lateral transshipments. In this paper, the authors select a three-site inventory system as the research object, and by introducing spares supply support relationship between sites, longitudinal and lateral transs...

Numerical simulation of effect of nozzle layout on jet lateral control for missiles
LIU Liyuan, LI Yachao, YAN Chao
2017, 43(8): 1632-1639. doi: 10.13700/j.bh.1001-5965.2016.0603
Abstract:

In order to keep the motility in the thin atmosphere, air vehicles usually employ reaction control system (RCS), but in supersonic flow, it leads to complex jet interaction flow field on the surface of air vehicles, which has enormous influence on flight control. In order to improve the regularity u...

Data association algorithm for unequal length sequence based on multiple model
SUN Guidong, GUAN Xin, YI Xiao, ZHAO Jun
2017, 43(8): 1640-1646. doi: 10.13700/j.bh.1001-5965.2016.0658
Abstract:

When dealing with data association for unequal length sequence, single model cannot balance computational accuracy, complexity and disturbance rejection. So a data association algorithm for unequal length sequence based on multiple model (MM) was proposed. The two unequal length sequence similarity ...

Finite element analysis of flow field and temperature field of electro-hydraulic pump by Fluent
FU Yongling, YANG Jiayuan, ZHU Deming
2017, 43(8): 1647-1653. doi: 10.13700/j.bh.1001-5965.2016.0605
Abstract:

The integrated structure and working principle of three phase induction motor-axial piston electro-hydraulic pump (EHP) were introduced. The mechanical losses were calculated. A model of EHP was established in Ansoft software, and then the electromagnetic losses were analyzed. Finite element couplin...

Demodulation error and influencing factor of three-wavelength digital phase demodulation method
ZHAO Wentao, SONG Ningfang, SONG Jingming, WU Rong
2017, 43(8): 1654-1661. doi: 10.13700/j.bh.1001-5965.2016.0568
Abstract:

This paper introduces the traditional demodulation method of Fabry-Perot (F-P) sensors, and systematically derives the demodulation principle of three-wavelength digital phase demodulation method using extrinsic Fabry-Perot interferometer (EFPI) sensors. Meanwhile, simulation method has been used to...

Reliability life prediction of smart meter based on multi-stress degradation model
ZHANG Jingyuan, HE Yuzhu, CUI Weijia
2017, 43(8): 1662-1669. doi: 10.13700/j.bh.1001-5965.2016.0582
Abstract:

Aimed at the difficulty to accurately predict the reliability life of smart meter in running state, based on the generalized multi-stress accelerated model, this study researched and determined the life distribution rules of smart meter by using the accelerated degradation test data. Through the ana...

Static aeroelastic characteristics analysis of high-aspect-ratio wing for hydrogen-powered UAV
HAO Shuai, MA Tielin, GAN Wenbiao, LI Gen
2017, 43(8): 1670-1676. doi: 10.13700/j.bh.1001-5965.2016.0611
Abstract:

Based on hydrogen-powered ultra-long endurance unmanned aerial vehicle (UAV), nonlinear static aeroelastic characteristics were analyzed by the strong-coupled method for its high-aspect-ratio light composite wing. The aerodynamic comparison of rigid and elastic (aeroelastic deformation) wing was inv...

Mechanical and dynamic characteristics of bearing with looseness on high-speed flexible rotor
YU Huan, MA Yanhong, XIAO Sen, HONG Jie
2017, 43(8): 1677-1683. doi: 10.13700/j.bh.1001-5965.2016.0635
Abstract:

Based on analysis of the structural and mechanical characteristics of the bearing with looseness on high-speed flexible rotor and the demand of dynamic optimal design for multi-supported flexible rotor, the mechanism of non-straight change of stiffness of supporting structure caused by looseness on ...

Transient communication signal detection under non-Gaussian noise based on improved HHT
GUO Xiaotao, WANG Xing, ZHOU Dongqing, ZHANG Ying
2017, 43(8): 1684-1692. doi: 10.13700/j.bh.1001-5965.2016.0576
Abstract:

Based on the characteristics of transient communication signals and non-Gaussian noise, the corresponding signal models were established, and a novel algorithm of transient communication signal detection under non-Gaussian noise was proposed based on the improved Hilbert-Huang transform (HHT), which...

Novel guidance law accounting for dynamics of missile autopilot
ZHANG Kai, YANG Suochang, ZHANG Kuanqiao, ZHANG Yongwei, CHEN Peng
2017, 43(8): 1693-1704. doi: 10.13700/j.bh.1001-5965.2016.0630
Abstract:

Interception of air targets requires zero miss-distance and impact angle constraint to improve the missile guidance performance. First, the acceleration of the target was estimated by extended disturbance observer which also considered the noise interference. Second, a nonsingular terminal sliding m...

Global sensitivity analysis under mixed uncertainty based on possibilistic moments
CHENG Kai, LYU Zhenzhou, SHI Yan
2017, 43(8): 1705-1712. doi: 10.13700/j.bh.1001-5965.2016.0626
Abstract:

For the structures with fuzzy uncertainty and random uncertainty simultaneously, to measure the influence of fuzzy and random input variables on the statistical characteristic of output response, a new global sensitivity index is proposed. Based on the definition of possibilistic moments of the fuzz...