2018 Vol. 44, No. 8

Display Method:
Volume 44 Issue82018
iconDownload (24298) 774 iconPreview
An algorithm for fast reconstruction of electromagnetic tomography images
LIU Ze, XIAO Jun, LIU Xianglong, ZHAO Pengfei, LI Yong, HUO Jiwei
2018, 44(8): 1569-1576. doi: 10.13700/j.bh.1001-5965.2017.0651
Abstract:

For the inverse problem of electromagnetic tomography (EMT), the pathological and ill posed problems of the sensitivity matrix are discussed. A new electromagnetic tomography image reconstruction algorithm is proposed for this situation. Firstly, the principal component analysis (PCA) is used to red...

Mechanism and experimental research on fluid flow in annulus of coaxial rotating conical cylinders
BAO Feng, ZENG Hualun, ZOU He, LIU Jinsheng, LIU Zhirong, ZHU Rui
2018, 44(8): 1577-1586. doi: 10.13700/j.bh.1001-5965.2017.0614
Abstract:

The research on the flow fluid in the annulus of coaxial rotating conical cylinders originates from the classical Taylor Couette flow in the annulus of two coaxial rotating conical cylinders. This paper uses flow visualization experiments and PIV to display and quantify the internal flow field in th...

Complex equipment risk conduction analysis based on UR-MTPGERT model
SUN Yun, WANG Ying, LI Chao
2018, 44(8): 1587-1595. doi: 10.13700/j.bh.1001-5965.2017.0800
Abstract:

Aimed at the problem of unclear description of the conduction relationship of complex equipment risks, a risk conduction uncertain random multi-transfer parameter graph evaluation and review technique (UR-MTPGERT) model is constructed. First, based on the opportunity theory, the moment function of u...

A thermodynamic modeling method of electro-hydrostatic actuator and law of oil temperature rise
WANG Yan, GUO Shengrong, YANG Le
2018, 44(8): 1596-1602. doi: 10.13700/j.bh.1001-5965.2017.0622
Abstract:

Electro-hydrostatic actuator (EHA), one of the key subsystems in the more electric aircraft, can reduce the size and weight of airborne equipment because of its highly compact design. However, the heat dissipation is weakened simultaneously, which can easily lead to an extremely rapid temperature in...

Control design and experimental verification of three-bed onboard oxygen generation system
JIANG Dongsheng, BU Xueqin, LIN Guiping, SUN Bing, HUANG Jun, FANG Ling, ZHAO Hongtao
2018, 44(8): 1603-1608. doi: 10.13700/j.bh.1001-5965.2017.0748
Abstract:

Two-bed onboard oxygen generation system is facing the problem of large pressure fluctuation of output gas and high oxygen concentration at low altitude during the practical application process. In order to solve these problems, three-bed onboard oxygen generation system needs to be developed. Accor...

A Web cache replacement strategy for spacecraft comprehensive testing system
DU Jianhai, LYU Jianghua, GAO Shiwei, LI Qianqian, LI Qinyong, MA Shilong
2018, 44(8): 1609-1619. doi: 10.13700/j.bh.1001-5965.2017.0591
Abstract:

As a typical safety critical system, spacecraft is generally a complex system, which could produce a large amount of test data during the comprehensive testing process.When querying these test data, the existing B/S data query technology obtains data from the database server for each query, which gr...

Impact factor weight analysis of atmospheric corrosion rate of carbon steel based on MIV
YANG Bin, LI Jingyang, WEN Lei
2018, 44(8): 1620-1628. doi: 10.13700/j.bh.1001-5965.2017.0638
Abstract:

Based on the mean impact value (MIV) which is an impact factor weight analysis method, the weights of fifteen impact factors on corrosion rate of four types of carbon steels (Q235, Ste355, St12, and Q450) were evaluated. The impact factors were corrosion duration, temperature, humidity, sunshine hou...

Aeroelastic optimization design of composite wing for large aircraft with panel stiffness matching
XIAO Zhipeng, QIAN Wenmin, ZHOU Lei
2018, 44(8): 1629-1635. doi: 10.13700/j.bh.1001-5965.2017.0613
Abstract:

A method of aeroelastic optimization design with consideration of panel stiffness matching was developed for the composite wing of large aircraft. The optimization was performed based on the sensitivity algorithm, and the objective was to minimize the structural mass subject to the constraints of pa...

Indoor TOA ranging value optimization method based on nonlinear programming
SUN Jian, FU Yongling, HE Jie, TAN Lin, LI Shengguang, XU Wenpeng
2018, 44(8): 1636-1642. doi: 10.13700/j.bh.1001-5965.2017.0641
Abstract:

The ranging accuracy of time of arrival (TOA) based indoor positioning system is significantly affected by multipath and non-line-of-sight (NLOS) of wireless channel in indoor environment. And these effects result in large measurement error and positioning error. In this paper, the optimization of d...

A method for quick measurement of terminal common-mode impedance of cables
LIU Hongyi, CHEN Yao, SU Donglin
2018, 44(8): 1643-1650. doi: 10.13700/j.bh.1001-5965.2017.0626
Abstract:

The cables connecting avionics equipment are important coupling path for electromagnetic interference. When modeling a cable, the terminal common-mode impedance of the cable is a crucial input parameter. Because the quantity of cables in avionics system is very large, it is beneficial for quickly mo...

Dynamic UCAVs cooperative task allocation based on SAGWO algorithm
WEI Zhenglei, ZHAO Hui, HUANG Hanqiao, WANG Xiaofei, ZHOU Rui
2018, 44(8): 1651-1664. doi: 10.13700/j.bh.1001-5965.2017.0589
Abstract:

Through analyzing unmanned combat aerial vechicle (UCAV) advantage probability and task joint threat and defining task time, the task allocation model for UCAVs with multi-constraint dynamic task allocation is built up, which takes target value damage, UCAV attrition and task expending time as the p...

A model of helicopter elastomeric damper for time varying amplitude analysis
WU Jing, HU Guocai, LIU Xiangyi
2018, 44(8): 1665-1671. doi: 10.13700/j.bh.1001-5965.2017.0633
Abstract:

The existing elastomeric damper models commonly introduce dynamic amplitude parameter for applying to wide amplitude situation. It is inconvenient to time domain analysis of helicopter rotor-fuselage coupled dynamic stability on account of the dynamic amplitude changing in time domain. Aimed at this...

Uncertainty evaluation for dynamic characteristic parameters of pressure sensors
YAO Zhenjian, WANG Zhongyu, WANG Chenchen, ZUO Siran
2018, 44(8): 1672-1681. doi: 10.13700/j.bh.1001-5965.2017.0636
Abstract:

The uncertainty of dynamic characteristic parameters of pressure sensors is an important index to characterize its dynamic measurement performance. A method is proposed to evaluate the uncertainty of the sensor's dynamic characteristic parameters. Firstly, a shock tube dynamic calibration system is ...

Simulation-based research on airflow organization for small data center
ZHOU Chenglong, YANG Chunxin, WANG Chao, ZHANG Xingjuan
2018, 44(8): 1682-1692. doi: 10.13700/j.bh.1001-5965.2017.0658
Abstract:

To allow small data center to work under the office environment to reduce the operating cost, an integrated design of noise reduction and refrigeration is proposed by combining the vapor compression refrigeration system with the server.Based on the verified simulation method of two key component, ax...

Localized multi-kernel diagnosis model for avionics based on affinity propagation clustering
ZHANG Wei, XU Aiqiang, PING Dianfa, XIA Fei
2018, 44(8): 1693-1704. doi: 10.13700/j.bh.1001-5965.2017.0632
Abstract:

In consideration of the low diagnosis accuracy for avionics functional module fault, a new offline localized clustering multi-kernel extreme learning machine (LCMKELM) diagnosis model is proposed in this paper by combining the capabilities of multi-resolution interpretation and local feature self-ad...

Static error model of a gyroscope with gas-dynamic hemispherical bearings
LI Yan, DUAN Fuhai
2018, 44(8): 1705-1711. doi: 10.13700/j.bh.1001-5965.2017.0570
Abstract:

In order to investigate the influence of deformation of gas film in gas-dynamic hemispherical bearings on the output of three-floated gyroscopes in the platform initial navigation system subject to 3-DOF specific forces, a mathematical model is established to calculate the static error by solving Re...

A kind of multistage transformable wheel for mobile robots
YANG Yang, CHANG Jungche, GUANG Chenhan, WANG Yang
2018, 44(8): 1712-1719. doi: 10.13700/j.bh.1001-5965.2017.0580
Abstract:

The transformable wheel is an effective way to enhance the wheeled mobile robots' obstacle navigation ability in harsh terrain. However, traditional single-structure transformable wheels can only adapt to specific environment and unable to simultaneously satisfy the environments with varieties of ha...

Corrosion sensitivity of 5A06 aluminum alloy welded samples under loading
WANG Shuai, LIU Huicong, LI Weiping, ZHU Liqun, SHI Wenjing, SHI Liming
2018, 44(8): 1720-1726. doi: 10.13700/j.bh.1001-5965.2017.0583
Abstract:

Aimed at the aluminum alloy welding effect on corrosion sensitivity, we have applied loading on the 5A06 aluminum alloy with the welds in different directions (vertical, cross) and studied the effects of stress loading on the corrosion behavior of the alloy in 3.5%NaCl solution at 50℃ and the electr...

Off-resonance laser frequency stabilization method for fast and accurate adjustment of frequency lock points
FANG Zishan, QUAN Wei, ZHAI Yueyang
2018, 44(8): 1727-1732. doi: 10.13700/j.bh.1001-5965.2017.0644
Abstract:

The atomic magnetometer and Raman cooling need to lock the frequency of the laser on the detuning of several gigahertz away from the resonance. The laser frequency stabilization technique in Faraday rotation spectroscopy can stabilize the laser frequency on the large detuning away from the resonance...

Adjustable-parameter dynamical decoupling protocol for 13C nuclear addressing in diamond
ZHANG Gangyuan, YUAN Heng, FAN Pengcheng
2018, 44(8): 1733-1738. doi: 10.13700/j.bh.1001-5965.2017.0652
Abstract:

A symmetric non-equally spaced protocol named adjustable-parameter dynamical decoupling (APDD) was proposed to individually map 13C nuclear spin in diamond. The principles of the APDD sequence are in detail numerically calculated and simulation analyzed. The 13C nuclear spin addressing accuracy of A...

Demonstration and verification system for UAV swarm formation control
ZHU Chuangchuang, LIANG Xiaolong, ZHANG Jiaqiang, HE Lyulong, LIU Liu
2018, 44(8): 1739-1747. doi: 10.13700/j.bh.1001-5965.2017.0600
Abstract:

In order to verify the effectiveness of the formation control algorithms of UAV swarm in the actual environment, a distributed UAV swarm formation control demonstration and verification system consisting of UAV platform, two sets of ground station and data link was built under outdoor conditions. Th...

Effect of acceleration on pilot operation in short-distance takeoff
ZHU Yuanjie, LIU Xiaoyu, GENG Xiaoqi, HUO Hongqiang, LIU Songyang, FAN Yubo
2018, 44(8): 1748-1754. doi: 10.13700/j.bh.1001-5965.2017.0573
Abstract:

Acceleration overlord during short-distance takeoff might affect the operation performance of pilot. To avoid potential risks, a pilot-cockpit multi-rigid-body model was established to simulate the man-machine dynamic response under chest-to-back (Gx) acceleration loads. Firstly, using 3D CAD softwa...

A new gyro torquer's non-circular error compensation method
CHEN Guoyue, WANG Hua, REN Yuan, XIN Chaojun
2018, 44(8): 1755-1763. doi: 10.13700/j.bh.1001-5965.2017.0604
Abstract:

Based on the structural design of the Lorentz force magnetic bearing (LFMB), a kind of torquer's non-circular error compensation method is put forward to enhance the sensitivity accuracy of magnetically suspended control sensitive gyroscope (MSCSG) to gyro carrier attitude. First, for a new type MSC...

In-depth data fusion of TOF and stereo vision system based on confidence level
SUN Zhe, ZHANG Yong, CHANG Qutong
2018, 44(8): 1764-1771. doi: 10.13700/j.bh.1001-5965.2017.0653
Abstract:

To solve the problem of 3D reconstruction in textureless environment like railway, the confidence coefficient is proposed to combine TOF and stereo vision system effectively. Through the joint calibration, the coordinate relationship between TOF and stereo vision systems is established. Then by proj...

Thermal structure analysis and simulation of solid-gelled propellant gas generator
LUO Yegang, XING Yuming, LIU Xin, LIANG Cai
2018, 44(8): 1772-1779. doi: 10.13700/j.bh.1001-5965.2017.0660
Abstract:

Solid-gelled propellant gas generator is a new and special gas generator, and is the core component of the variable-depth missile ejection system. In order to study the temperature distribution of storage space of solid-gelled propellant gas generator, the source term method, the dynamic mesh method...

Design and analysis of an aluminum alloy bus frame under typical conditions
WANG Kai, HE Yongling, MENG Guangwei
2018, 44(8): 1780-1786. doi: 10.13700/j.bh.1001-5965.2017.0656
Abstract:

Lightweight materials such as high-strength steel, aluminum alloy or magnesium alloy applied as substitutions of plain steel to manufacture of bearing structures on vehicle have been an obvious tendency. Using industrial aluminum alloy as material, a new light bus frame was designed in this paper, a...