2017 Vol. 43, No. 7

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A calculation method for temperature control orifice of ram air turbine pump
WANG Yan, YIN Yafeng, CHEN Jinhua, JIANG Pei
2017, 43(7): 1287-1292. doi: 10.13700/j.bh.1001-5965.2016.0545
Abstract:

Ram air turbine (RAT) pump, by transforming the mechanical energy into hydraulic energy, can be used to control the aircraft rudder in emergency situation. Its performance of rapid response is critical to ensure the aircraft's safety. Exposed to low-temperature atmosphere for long time, the high vis...

Improved test method based on vector cancellation for scattering characteristic of discontinuous target
GAO Xu, YANG Shuo, CHAI Jianzhong, ZHAO Jingcheng
2017, 43(7): 1293-1299. doi: 10.13700/j.bh.1001-5965.2016.0517
Abstract:

For stealth aircraft, the scattering contribution of discontinuous targets becomes considerable. The common method is based on low scattering carrier and compares measurement results of carrier with discontinuity and that without discontinuity. The scattering increase of target with discontinuity is...

Measurement for back-reflection of photonic crystal fiber fusion splicing point based on low-coherence light
XU Xiaobin, YAN Ming, TENG Fei, WU Chunxiao
2017, 43(7): 1300-1305. doi: 10.13700/j.bh.1001-5965.2016.0499
Abstract:

Although angle-cleaved fusion splice can greatly reduce the reflection of the fusion splicing point between photonic crystal fiber (PCF) and conventional single mode fiber, a weak residual back-reflection still exists at the fusion splicing point. A Mach-Zehnder and Michelson hybrid interferometer b...

Flight management system redundancy optimization method based on genetic algorithm
HUO Lin, FEI Simiao
2017, 43(7): 1306-1312. doi: 10.13700/j.bh.1001-5965.2016.0512
Abstract:

Aircraft management system is an important part to guarantee flight safety, and redundancy design is the main method to improve the safety of the system. The redundancy design, however, is constrained by the budget (economy) in the design and manufacture and the consumption of the maintenance suppor...

Enhanced resolution in MIMO-SAR imaging using apodization
XU Guangyao, LIU Yongze, XU Xiaojian
2017, 43(7): 1313-1320. doi: 10.13700/j.bh.1001-5965.2016.0514
Abstract:

When the conventional methods of sidelobe suppression are used in multiple input multiple output synthetic aperture radar (MIMO-SAR) systems to generate images for diagnosing the near field scattering features of targets, non-orthogonal sidelobes can hardly be suppressed efficiently. In this paper, ...

Quasi-variational principle and application of initial value problem for rigid-elastic coupling dynamics
ZHOU Ping, LI Haibo, LIANG Lifu
2017, 43(7): 1321-1329. doi: 10.13700/j.bh.1001-5965.2016.0849
Abstract:

The rigid-elastic coupling dynamics has been widely used in the national defense and civil economic construction, but there are still no mature theoretical research results. In this view, the quasi-variational principle of the initial value problem was established, according to rigid-elastic couplin...

Common-path confocal interferometric surface plasmon microscopy
ZHANG Bei, YAN Peng, WANG Le, GAO Feng, YUAN Mei
2017, 43(7): 1330-1335. doi: 10.13700/j.bh.1001-5965.2016.0526
Abstract:

Surface plasmon (SPs) microscopy can measure local changes of refractive index on the nano scale and has been successfully applied in biomedical or semiconductor material fields. Here, we propose and develop a novel common-path confocal interferometric SPs microscopy. This technique delivers quantit...

Circuitry test response signal reconstruction based on GP-KSVD algorithm
NIE Jing, SU Donglin, LI Hongyi, ZHAO Di
2017, 43(7): 1336-1347. doi: 10.13700/j.bh.1001-5965.2016.0518
Abstract:

Response signals in circuitry system always have the characteristics of high periodicity and sparse distribution. In order to realize response signals reconstruction in circuitry system, an algorithm combining gradient pursuit and K singular value decomposition (GP-KSVD) was proposed. Dictionary was...

Quantified effects of high-altitude wind on route performance of large passenger plane
HUANG Chengtao, WANG Lixin, ZHONG Bowen
2017, 43(7): 1348-1354. doi: 10.13700/j.bh.1001-5965.2016.0542
Abstract:

High-altitude wind affects the fuel consumption and flight time of large passenger plane route flight. This paper is aimed at proposing a method to calculate the route performance of aircraft in high-altitude wind, and analyzing the effects of high-altitude wind on route performance of large passeng...

A calculation method for power supply capability of spacecraft solar array
LI Tao, LI Wei, YANG Lei
2017, 43(7): 1355-1363. doi: 10.13700/j.bh.1001-5965.2016.0600
Abstract:

The solar array supplies power to spacecraft. Thus, it is important to predict power supply capability for spacecraft design and certification of on-orbit flight operation, and a calculation method for power supply capability of spacecraft solar array is proposed. The current versus voltage model of...

Visual object tracking based on objectness measure with multiple instance learning
HUA Weixin, MU Dejun, GUO Dawei, LIU Hang
2017, 43(7): 1364-1372. doi: 10.13700/j.bh.1001-5965.2016.0527
Abstract:

For the problems that the multiple instance learning (MIL) tracking algorithm does not distinguish the differences of each sample when computing the bag probability and selects the weak classifiers by maximizing the log likelihood function, which reduce the performance of classifier and increase the...

Plasma assisted methane ignition under different diluent gas
SHEN Shuangyan, JIN Xing, DENG Tongye
2017, 43(7): 1373-1379. doi: 10.13700/j.bh.1001-5965.2016.0544
Abstract:

Plasma could increase chemical and heat effect at the same time during the fuel reaction and it is expected to be an effective technical way of ignition assistance. Plasma assisted methane ignition experiment system was built based on shock tube. The methane ignition delay time of autoignition, unde...

Exit burr in rotary ultrasonic-assisted drilling of titanium alloys
LI Zhe, ZHANG Deyuan, JIANG Xinggang
2017, 43(7): 1380-1386. doi: 10.13700/j.bh.1001-5965.2016.0556
Abstract:

In aerospace industries, to solve the problem of big exit burr which leads to the difficulty in deburring operations and poor assembly quality of fastener after the traditional drilling process of the difficult-to-cut materials like titanium alloys using a twist drill, the rotary ultrasonic-assisted...

Micro-motion classification of spatial cone target based on micro-Doppler
SHU Changyong, ZHANG Shengjun, HUANG Peilin, JI Jinzu
2017, 43(7): 1387-1394. doi: 10.13700/j.bh.1001-5965.2016.0500
Abstract:

There are many kinds of micro-motion in the spatial cone target in flight, which can be divided into nutation, precession and spinning. Accurate acquisition of the target's micro-motion form is the premise for the estimation of the micro-motion and the structural parameters of the ballistic target. ...

Deformation behavior of a bent tube based on free expansion
KONG Deshuai, LANG Lihui, RUAN Shangwen
2017, 43(7): 1395-1402. doi: 10.13700/j.bh.1001-5965.2016.0525
Abstract:

As the development of lightweight design in manufacture industry, the application of thin-walled bent hollow tubes with various sections is expanding widely. In order to study the deformation behavior of bent tubes during hydroforming process and have a reliable process design, a theoretical model o...

Reliability modeling method for security & protection system of a key area
ZHA Guoqing, XU Yani, KANG Rui
2017, 43(7): 1403-1409. doi: 10.13700/j.bh.1001-5965.2016.0905
Abstract:

In order to evaluate the reliability of a security system in the key area, security system reliability of a key area is defined in this paper firstly. Failure distributions of security devices are acquired after the test and estimation of security devices' failure information by exponential distribu...

Separation flow and blade dynamic response characteristic of compressor at high attack angle
NI Qifeng, HOU Anping, LIU Ruoyang, ZHOU Baihao, ZHANG Mingming
2017, 43(7): 1410-1418. doi: 10.13700/j.bh.1001-5965.2016.0912
Abstract:

In order to study the shedding and propagation of compressor rotors at high angle of attack, as well as the dynamic response under this transient process, a model with a stage of transonic compressor was simulated with unsteady numerical method and double direction iteration fluid-structure coupled ...

Immune SVM used in wear fault diagnosis of aircraft engine
ZHANG Jian, LI Yanjun, CAO Yuyuan, ZHANG Lina
2017, 43(7): 1419-1425. doi: 10.13700/j.bh.1001-5965.2016.0553
Abstract:

Aircraft engine is wearing during its service life and will finally break down. The wear fault can be diagnosed by analyzing the ferrography data of oil monitoring. The use of immune algorithm optimized support vector machine (SVM) in aircraft engine wear fault diagnosis was researched in this paper...

A collaborative localization algorithm based on non-line-of-sight error compensation
ZHANG Ran, SONG Lailiang, RAN Longjun
2017, 43(7): 1426-1432. doi: 10.13700/j.bh.1001-5965.2016.0557
Abstract:

The non-line-of-sight (NLOS) error has great influence on the positioning accuracy of the ultra-wideband (UWB) indoor positioning technology. Aimed at this problem, this paper estimates the mean and variance of NLOS according to the joint statistical properties of the additional time delay in NLOS a...

Metal structure crack monitoring based on copper film sensor in corrosion environment
TAN Xiangfei, HE Yuting, HOU Bo, CUI Ronghong, FENG Yu
2017, 43(7): 1433-1441. doi: 10.13700/j.bh.1001-5965.2016.0534
Abstract:

In the process of monitoring aircraft metal structure crack, copper film sensor is exposed to atmospheric corrosion environment. The corrosion resistance of copper film sensor and crack monitoring performance after corrosion experiment were researched under the background. First, copper films were d...

End-to-end traffic latency computation using frame shaping model in AVB network
LI Ershuai, HE Feng, XIONG Huagang
2017, 43(7): 1442-1449. doi: 10.13700/j.bh.1001-5965.2016.0539
Abstract:

Audio video bridging (AVB) Ethernet is an available Ethernet-based solution for audio and video stream transmissions within embedded networking context, in which credit-based shaping (CBS) algorithm is defined to guarantee the end-to-end latency performance according to stream models. When consideri...

Close-range air combat situation assessment using deep belief network
ZHANG Binchao, KOU Yanan, WU Meng, ZUO Jialiang
2017, 43(7): 1450-1459. doi: 10.13700/j.bh.1001-5965.2016.0956
Abstract:

Considering the difficulty in parameter setting, weakness of traditional situation assessment methods in processing and feature extraction of big data, feature of air combat data, applications of deep belief network (DBN) to close-range air combat situation assessment are discussed. A sample library...

Uncertainty analysis of failure of dynamic system and its efficient algorithm
GONG Xiangrui, LYU Zhenzhou, LIU Hui, ZHOU Yicheng
2017, 43(7): 1460-1469. doi: 10.13700/j.bh.1001-5965.2016.0533
Abstract:

In order to study the failure of dynamic system when the failure rates of components are uncertain, a new method is proposed to analyze the system failure probability when function time is given and function time when the threshold of failure probability is shown in system. Meanwhile, a new importan...

Model validation method with multivariate output based on kernel principal component analysis
HU Jiarui, LYU Zhenzhou
2017, 43(7): 1470-1480. doi: 10.13700/j.bh.1001-5965.2016.0519
Abstract:

At present, for the multiple correlated complex computational models with uncertainty, the traditional validation methods still have some problems, such as difficult calculation and poor stability.Aimed at such complex computational models, a new multivariate model validation method is proposed base...

Path following method with adaptive guidance length for unmanned aerial vehicles
LI Yue, CHEN Qingyang, HOU Zhongxi
2017, 43(7): 1481-1490. doi: 10.13700/j.bh.1001-5965.2016.0522
Abstract:

To guarantee the flight stability and high accuracy of path following for unmanned aerial vehicles (UAVs), a nonlinear path following method with adaptive guidance length is proposed. First, the kinematic model of UAVs was built. Second, the relation between guidance length and velocity of UAVs was ...

Study of supersonic flow field control mechanism with micro jet
LIU Pingchao, LIU Yanming, CHEN Sicheng, QIN Yang
2017, 43(7): 1491-1500. doi: 10.13700/j.bh.1001-5965.2016.0515
Abstract:

An numerical investigation was conducted to study the influence of micro jet with different total injection pressure on the supersonic flow field (Ma=2.9) for a 24° compression corner. The ejecting direction is vertical to incoming flow. The results show that the velocity of the fluid downstream the...