2016 Vol. 42, No. 12

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Fuel control law of small size turbofan engine
SU Zhigang, ZHANG Lingxiao, DENG Tian
2016, 42(12): 2555-2562. doi: 10.13700/j.bh.1001-5965.2015.0829
Abstract:

Focusing on the fuel control law of the small size turbofan engine DGEN380, a steady and transient component-level mathematical model was developed and simulated on MATLAB platform with analytic method. A special tool was used for modeling the rotating parts in order to get the components characteri...

Strictly regular random (3, s)-SAT model and its phase transition phenomenon
ZHOU Jincheng, XU Daoyun, LU Youjun, DAI Cunkuan
2016, 42(12): 2563-2571. doi: 10.13700/j.bh.1001-5965.2015.0845
Abstract:

We study the restricted occurrence times for variables and literatures in 3-SAT problem. In particular, we propose a strictly regular random (3, s)-SAT problem and its instances generating model-SRR model. Using the first moment method and the asymptotic approximation technique to the expansion coef...

Receiver autonomous integrity monitoring based on particle swarm optimization particle filter
WANG Ershen, QU Pingping, PANG Tao, LAN Xiaoyu, CHEN Jiamei
2016, 42(12): 2572-2578. doi: 10.13700/j.bh.1001-5965.2016.0362
Abstract:

Receiver autonomous integrity monitoring (RAIM) is an inseparable part of aviation satellite navigation receiver. Failures or faults due to malfunctions in the global navigation satellite system (GNSS) should be detected and isolated to keep the integrity of the GNSS intact. Because measurement nois...

Dynamic bandwidth allocation mechanism with parallel and switching for FC-AE-1553 network
WU Shaojun, ZHAO Guangheng, WANG Liqian, ZHAN Yueying, WANG Jin, WANG Hongxiang
2016, 42(12): 2579-2586. doi: 10.13700/j.bh.1001-5965.2015.0856
Abstract:

In order to meet the requirement of space payload system and data transmission, the data business type was divided into periodic business, burst business and strong timeliness business. After the characteristics of the three kinds of business are analyzed, a scheme of dynamic bandwidth allocation (D...

Hypersonic vehicle shape optimal design based on overall performance
DENG Fan, JIAO Zihan, FU Qiujun, CHEN Lin, TIAN Shuling, ZHANG Dong
2016, 42(12): 2587-2595. doi: 10.13700/j.bh.1001-5965.2015.0847
Abstract:

Aerodynamic configuration design and optimization are vital to overall design of aircraft. Higher requirements of lift-drag ratio and control performance are put forward for near space vehicles. The lifting-body shape of the wing-body combination has become the main design direction of the hypersoni...

Soft robot system based on intelligent driver
SHI Zhenyun, ZHU Qiancheng
2016, 42(12): 2596-2602. doi: 10.13700/j.bh.1001-5965.2015.0804
Abstract:
Soft robot, as a new type of flexible robot, is attracting more and more attention. How to build emergency ability in unpredictable environments is the key research goal of soft robot technology. For this problem, an intelligent driving-sensing based motion pattern and system component of semi-soft ...
Effect of wing-tip trajectory on aerodynamics of hovering true hoverfly
MOU Xiaolei, XU Na
2016, 42(12): 2603-2609. doi: 10.13700/j.bh.1001-5965.2015.0843
Abstract:

For the hovering true hoverfly, stroke deviation angle is relatively small. It is higher at the beginning and end of a downstroke or upstroke, and lower at the middle of the downstroke or upstroke, which leads to a shallow U-shaped wing-tip trajectory. In order to investigate the effect of wing-tip ...

Storage degradation testing and life prediction for missile electromagnetic relay
WANG Zhaobin, FU Sai, SHANG Shang, ZHAI Guofu
2016, 42(12): 2610-2619. doi: 10.13700/j.bh.1001-5965.2015.0789
Abstract:

Missile electromagnetic relay (EMR) is one of the key electromechanical components used for signal transmission, load switching and circuit protection in defense weapon system. How to reliably evaluate the storage reliability of missile EMR has become the most important problem that is urgent to be ...

Stray light suppressing technique and simulation for star sensor
LI Yang, LIAO Zhibo, MU Shengbo, ZHANG Tingcheng
2016, 42(12): 2620-2624. doi: 10.13700/j.bh.1001-5965.2015.0793
Abstract:

Star sensor used for deep space stars exploration is a faint signal detector. Star sensor is sensitive to slender stray light, and therefore, the stray light suppressing ability is a key influencing factor of the exploration ability. Through the point source transmittance (PST), the suppression indi...

Deployment accuracy analysis of planar satellite antenna with joint clearances
DING Jianzhong, WANG Chunjie
2016, 42(12): 2625-2631. doi: 10.13700/j.bh.1001-5965.2015.0808
Abstract:

Planar folding satellite antenna deployment mechanism is widely used in the field of astronautics. It has a large and complicated topology structure, which is composed by joint-connecting rods. The existence of joint clearances makes the analysis of the antenna deployment a tough task and contribute...

Convex surface ray tracing based on adaptive cutting surface adjustment under exact normal vector
LI Yaoyao, SU Donglin, LIU Yan, YANG Zhao
2016, 42(12): 2632-2639. doi: 10.13700/j.bh.1001-5965.2016.0442
Abstract:

Electrical large targets are difficult to be accurately and analytically expressed and thus it is difficult to use uniform geometrical theory of diffraction (UTD) method for field computation. Aimed at this problem, a novel creeping ray triangular mesh tracing (TM-tracing) algorithm for arbitrary co...

Modeling of hypersonic vehicle via model migration method
WANG Haoliang, LI Qingdong, REN Zhang, ZHAO Qilun, DONG Xiwang, LIU Fei
2016, 42(12): 2640-2647. doi: 10.13700/j.bh.1001-5965.2015.0807
Abstract:

The development of hypersonic vehicle is a process of multi-product and small-batch production. In order to reduce the cost of experiments and decrease the period of the modeling of hypersonic vehicles, model migration method is used to calculate the aerodynamic parameters of the vehicles with simil...

Minor loop dynamic Jiles-Atherton model in giant magnetostrictive actuator
GAO Xiaohui, LIU Yongguang, PEI Zhongcai
2016, 42(12): 2648-2653. doi: 10.13700/j.bh.1001-5965.2015.0815
Abstract:

Hysteresis nonlinear relationship between input and output exists in giant magnetostrictive actuator (GMA). In order to lower hysteresis nonlinearity of material, minor hysteresis loops are often applied when the high frequency characteristics are studied. Therefore, it is very important to research...

Cavitation performance of inducer with helical static blades
LI Xin, LI Jiawen, WANG Jue, LIU Zhongxiang
2016, 42(12): 2654-2661. doi: 10.13700/j.bh.1001-5965.2015.0818
Abstract:

In order to study internal flow pattern, the 3D flow in inducer with helical static blades is numerically computed by using the computational fluid dynamics (CFD). The suction and cavitation performance of the inducer are analyzed. The results show that the head increases with helical static blades,...

Stress concentration analysis of honeycomb with missing cell walls
SHI Xiaofei, XI Ping, SONG Yuwang, LI Ru, SHI Xiaojuan
2016, 42(12): 2662-2668. doi: 10.13700/j.bh.1001-5965.2015.0819
Abstract:

A kind of defect with some of the cell walls missing in a honeycomb structure causes the loss of continuum of the honeycomb, and thus results in the stress concentration around the defect tip. Combined with the finite element and the analytic methods, this paper analyzed the normal stresses distribu...

Numerical simulation to static ground effect of delta wings with different sweep angles
QIN Yunpeng, LIU Peiqing, QU Qiulin, HUANG Liewei
2016, 42(12): 2669-2675. doi: 10.13700/j.bh.1001-5965.2015.0844
Abstract:

In this paper, the static ground effect of delta wings with different sweep angles is investigated by numerical simulation. The analyses of aerodynamic force and flow field characteristics show that in ground effect, the "block effect" of ground enhances the windward surface pressure; with the sweep...

Experimental research of 1+3/2 contra-rotating turbine aerodynamic performance
WU Zhongye, FANG Xiangjun, LIU Siyong, ZHAO Dayong
2016, 42(12): 2676-2682. doi: 10.13700/j.bh.1001-5965.2015.0849
Abstract:

Vaneless contra-rotating turbine is one of the key technologies of the high performance engine. Experimental research was conducted to investigate aerodynamic performance of 1+3/2 contra-rotating turbine. The experiment was tested over three phases:first the alone high pressure turbine (HPT) experim...

Multimodal data fusion model for smart city
ZHANG Yi, CHEN Yujun, DU Bowen, PU Juhua, XIONG Zhang
2016, 42(12): 2683-2690. doi: 10.13700/j.bh.1001-5965.2015.0858
Abstract:

With the rapid growth of cloud computing and big data, in addition to the urgent demand for city development, smart city construction has become one of the hot topics of domestic and international computer science researches. With the increasing number of closed-circuit televisions and sensor device...

Effects of perturbation geometry on behavior of asymmetric flow over blunt body
QI Zhongyang, WANG Yankui, SHA Yongxiang, WANG Lei
2016, 42(12): 2691-2697. doi: 10.13700/j.bh.1001-5965.2015.0861
Abstract:

The asymmetric vortices can be determined through setting the artificial perturbation on the nose of the blunt body at high angle of attack. To study the influence of perturbation geometry on the asymmetric vortices, numerical simulation was applied and the hemispherical, D-type and square perturbat...

Movement rule of a vehicle obliquely water-entry at low speed
LI Yongli, FENG Jinfu, QI Duo, YANG Jian, HU Junhua, XU Baowei
2016, 42(12): 2698-2708. doi: 10.13700/j.bh.1001-5965.2016.0153
Abstract:

This paper proposes a single control strategy to solve the problem of difficult transmedia vehicle control. The proposed control strategy is just to control the vehicle's air navigation, but not to control the underwater navigation. The hydrodynamic model of a vehicle obliquely water-entry at low sp...

Fast calibration method for phased array antenna
WANG Huanju, SUN Houjun
2016, 42(12): 2709-2714. doi: 10.13700/j.bh.1001-5965.2015.0828
Abstract:

The study of rapid measurement and calibration for phased array antenna has always been one of hot issues. The low efficiency of traditional calibration method cannot satisfy the requirement of large-scale engineering application of phased array antenna. A fast calibration method called four-phase-c...

Development of a generalized surface partition and projection system for missile radome
LI Zhengzhou, XIAO Tianhang, ANG Haisong, LU Zhaoyan
2016, 42(12): 2715-2721. doi: 10.13700/j.bh.1001-5965.2015.0839
Abstract:

To meet the technical requirements of missile radome frequency selective surface (FSS), a partition and projection system of radome surface was proposed and developed. Based on the study of approximate partition and projection of complex surface, the partition coefficient was defined as the ratio of...

Dynamic priority scheduling algorithm for air defense phased array radar in overload situations
ZHANG Haowei, XIE Junwei, SHI Junpeng, LI Jingqing, SHENG Chuan
2016, 42(12): 2722-2729. doi: 10.13700/j.bh.1001-5965.2015.0779
Abstract:

Aimed at time resource allocation in the air defense phased array radar in overload situations, a new scheduling algorithm using the threat density of targets and deadline of tasks to decide the task dynamic priority was proposed. The nonlinear threat level of targets model was established and the d...

Corner building method and algorithm of automatic programing for aircraft structural parts
CUI Zhiwei, ZHENG Guolei
2016, 42(12): 2730-2737. doi: 10.13700/j.bh.1001-5965.2015.0810
Abstract:

Aimed at the problems of inefficiency, heavy work and unstable quality in corner numerical control (NC) programing for aircraft structural parts, a new auto-extended method based on rounded corner face was put forward. Combined with process knowledge, the processing model of corner is set up, which ...

Critical angle of revolute pin joint and its application in a four-bar mechanism
ZHANG Jie, WANG Dan, CHEN Wuyi
2016, 42(12): 2738-2744. doi: 10.13700/j.bh.1001-5965.2015.0812
Abstract:

Revolute pin joint (revolute pair) possesses one degree of freedom, i.e. rotation movement, through relative sliding between contact pairs. Existence of friction and clearance in revolute joints has crucial effects on the overall precision of mechanism. Using the concept of critical angle, the margi...

UAV 3D real-time path planning based on dynamic step
ZHANG Shuai, LI Xueren, ZHANG Jianye, ZHANG Peng, LI Bo, ZHAO Xiaolin
2016, 42(12): 2745-2754. doi: 10.13700/j.bh.1001-5965.2015.0821
Abstract:

Because planning unmanned aerial vehicle (UAV) path directly in 3D space is difficult, we divide 3D path planning into 2D plane path planning and height planning, and then combine them to get the 3D path so that planning space is simplified and complexity is reduced. To search the path subtly in the...

High squint helicopter-borne terahertz ViSAR vibration compensation imaging algorithm
SUN Wei, SUN Jinping, ZHANG Yuan, ZHANG Yaotian
2016, 42(12): 2755-2761. doi: 10.13700/j.bh.1001-5965.2015.0862
Abstract:

With advantages such as fast imaging frame rate, high resolutions and penetration through dust and smoke, video synthetic aperture radar (ViSAR) has a broad application prospect. But for ViSAR that works in terahertz carrier frequency, helicopter platform's tiny high frequency vibration will cause o...

Modeling and machanical properties of composite bionic suture joint structures
MAO Wei, WANG Wenzhi, HE Lijun, ZHANG Chao
2016, 42(12): 2762-2768. doi: 10.13700/j.bh.1001-5965.2015.0772
Abstract:

In this paper, we developed a parametric modeling framework for composite bionic suture joint structures through MATLAB and ABAQUS secondary development based on Python language. It shows the capability in describing the complicated suture joint geometry with different types of hierarchy and automat...