2018 Vol. 44, No. 10

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Numerical simulation of drop capturing capabilities on heterogeneous walls
ZHANG Ying, LU Min, LI Peisheng, XU Shufang, LIU Qiang, HUANG Jie
2018, 44(10): 2021-2027. doi: 10.13700/j.bh.1001-5965.2017.0799
Abstract:

In order to study the drop capturing capabilities of heterogeneous walls, a numerical method is developed by integrating the generalized Navier boundary condition into front tracking method (FTM) to establish the contact angle model. The numerical simulation of the movement of drops on the heterogen...

Simulation analysis of ion thruster plume thermal effect
ZHANG Jianhua, LI Jinghua, YOU Fengyi, ZHENG Hongru
2018, 44(10): 2028-2034. doi: 10.13700/j.bh.1001-5965.2017.0802
Abstract:

The plume ejected from a working ion thruster collides with the surface of spacecraft, which may cause thermal effects such as thermal deformation of the sensitive material and lead to the failure of the space mission in severe cases. In this paper, the plume thermal effect of LIPS-200 ion thruster ...

Effect of flow stress calculation on formability of aluminum alloy warm sheet hydroforming
CAI Gaoshen, WU Chuanyu, LANG Lihui, GAO Zepu
2018, 44(10): 2035-2042. doi: 10.13700/j.bh.1001-5965.2018.0025
Abstract:

In order to research the influence of flow stress calculation on formability of aluminum alloy warm sheet hydroforming, warm sheet bulging test was carried out to obtain bulging height-pressure curves with different bulging diameters in this study. Based on the data of bulging parts profile measured...

Direct torque control of switched reluctance motor based on adaptive second-order terminal sliding mode
LIU Yongzhi, SHAN Chenglong, LIN Bowen, SONG Jinlong
2018, 44(10): 2043-2051. doi: 10.13700/j.bh.1001-5965.2017.0781
Abstract:

The torque ripple of switched reluctance motor (SRM) can be reduced to some extent by traditional direct torque control (DTC), but the torque ripple suppression effect is poor in the commutation zone. And the traditional PI control has disadvantages of large overshoot, poor robustness and limited an...

Lubrication characteristics analysis of a type of self-cooling structure fuel pump sliding bearings
FU Jiangfeng, LI Huacong, FAN Ding, LIU Xianwei, ZHU Jiaxing, LI Kun
2018, 44(10): 2052-2062. doi: 10.13700/j.bh.1001-5965.2017.0762
Abstract:

The aim of this paper was to study the lubrication characteristics of sliding bearings for aeroengine fuel gear pumps under low medium viscosity and self-cooling conditions. Based on the Reynolds equation for hydrodynamic lubrication of oil film and equivalent viscosity lubrication flow model, the e...

RBF neural network tuning PID control based on UMAC
LI Ming, FENG Hang, ZHANG Yanshun
2018, 44(10): 2063-2070. doi: 10.13700/j.bh.1001-5965.2017.0777
Abstract:

The self-adaptability and robustness of traditional PID control and current fuzzy-PID control adopted by universal motion and automation controller (UMAC) were not strong, and the static-dynamic performance of servosystem controlled by them was not ideal. In this paper, RBF neural network was adopte...

Threat evaluation method of air target based on information entropy and rough set
YANG Yuanzhi, ZHOU Zhongliang, LIU Hongqiang, KOU Tian, FAN Xiangyu
2018, 44(10): 2071-2077. doi: 10.13700/j.bh.1001-5965.2017.0768
Abstract:

Aimed at the problem that rough set (RS) theory cannot deal with information system without decision when evaluation issues are processed, an air target threat evaluation model based on information entropy (IE) and RS is put forward. The model adopts IE method to calculate the attribute weights, cho...

Status and evaluation method of surface tactile representation technology
YAN Xuezhi, LI Ruige, WU Qiushuang
2018, 44(10): 2078-2095. doi: 10.13700/j.bh.1001-5965.2017.0790
Abstract:

Surface tactile representation technology can display characteristics of the displayed contents through our bare fingers, realizing efficient and natural interaction on multimedia terminal screens. However, most studies in this field focus on the force tactile interaction device, and do not systemat...

Dynamics modeling and kinematics calculation of webbed-feet during cormorant's take-off
GONG Xiao, HUANG Jinguo, CHEN Hongyu, WANG Tianmiao, LIANG Jianhong
2018, 44(10): 2096-2105. doi: 10.13700/j.bh.1001-5965.2018.0030
Abstract:

The process of taking off from the surface of water for cormorant is a combination of flapping its wings and its webbed-feet periodically. In order to look into the contribution of the latter that helps in taking off and to compute each period in fixed quantity of the amount of force in each flappin...

Test of ice shedding on turbofan engine blade in refrigeratory environment
CHEN Gong, YANG Kun, WANG Liping, KONG Weiliang, WANG Fuxin
2018, 44(10): 2106-2114. doi: 10.13700/j.bh.1001-5965.2018.0035
Abstract:

Due to the complexity and randomness of the turbofan blade icing shedding characteristics, it is difficult to use computational simulation to obtain reliable results. On the other hand, icing wind tunnel test can hardly be always applied due to its high cost. In this paper, a feasible, economical an...

A fault tolerant high-performance reduction framework in complex environment
LI Chao, ZHAO Changhai, YAN Haihua, LIU Chao, WEN Jiamin, WANG Zengbo
2018, 44(10): 2115-2124. doi: 10.13700/j.bh.1001-5965.2017.0786
Abstract:

Reduction is one of the most commonly used collective communication operations for parallel applications. There are two problems for the existing reduction algorithms:First, they cannot adapt to complex environment. When interferences appear in computing environment, the efficiency of reduction degr...

Path planning method for traction system on carrier aircraft
ZHANG Jing, WU Yu, QU Xiangju
2018, 44(10): 2125-2133. doi: 10.13700/j.bh.1001-5965.2017.0787
Abstract:

A carrier aircraft moves on a carrier flight deck which has the characteristics of heavy workloads and multiple obstacles. In order to reduce energy consumption of the carrier aircraft and improve service life of the aircraft engine, the carrier aircraft is usually dragged by a tractor on the flight...

Zonal behavior of angle of attack effects on vortices over blunt-slender body
QI Zhongyang, WANG Yankui, CAO Peng
2018, 44(10): 2134-2140. doi: 10.13700/j.bh.1001-5965.2018.0798
Abstract:

In order to achieve the high maneuverability of the air-to-air missile, the flow characteristics of vortices over the blunt-slender body at different angles of attack were studied by wind tunnel forces and pressure test in this paper. The Reynolds number is set as ReD=1.54×105, based on oncoming fre...

Deorbit planning of reentry vehicles using ground track manipulation
SHI Shufeng, SHI Peng, ZHAO Yushan
2018, 44(10): 2141-2148. doi: 10.13700/j.bh.1001-5965.2018.0107
Abstract:

Aimed at the deorbit problem of reentry vehicles with constraints of reentry point location, a deorbit planning method using ground track manipulation is proposed in this paper. The deorbit trajectory design of reentry vehicles is constrained by the parameters of the real-time orbit and the aimed re...

Performance analysis and parameter optimization of lander with variable damping buffer
LIU Xueao, WU Hongyu, WANG Chunjie, DING Zongmao, DING Jianzhong
2018, 44(10): 2149-2155. doi: 10.13700/j.bh.1001-5965.2017.0805
Abstract:

In order to analyze soft landing performance of typical legged lander with variable damping buffer, the dynamic simulation model of lander was established. Based on the simulation model, the soft landing performance of the lander in the uncertain landing environment was analyzed by using Monte Carlo...

Multi-model estimation of HGV based on coupled aerodynamic parameters
ZHANG Kai, XIONG Jiajun, FU Tingting, XI Qiushi
2018, 44(10): 2156-2164. doi: 10.13700/j.bh.1001-5965.2018.0028
Abstract:

Using aerodynamic parameters to model the unknown aerodynamics is an effective way to improve the tracking accuracy of hypersonic gliding vehicles. The aerodynamic acceleration and its derivative is analyzed to prove the necessity of unknown aerodynamics modeling in this paper. Based on the non-coup...

Fuel-optimal attitude maneuver using linear pseudo-spectral model predictive control method
FENG Yijun, CHEN Wanchun, YANG Liang
2018, 44(10): 2165-2175. doi: 10.13700/j.bh.1001-5965.2017.0770
Abstract:

In order to perform large angle attitude maneuvers of spacecraft outside the atmosphere, we propose a fuel-optimal large angle attitude maneuver strategy using modified linear pseudo-spectral model predictive control method. First, a fuel-optimal attitude maneuver trajectory satisfying initial and t...

Comparative study of variable amplitude multiaxial fatigue life analysis methods
LIU Tianqi, SHI Xinhong, ZHANG Jianyu, FEI Binjun
2018, 44(10): 2176-2184. doi: 10.13700/j.bh.1001-5965.2017.0782
Abstract:

Three commonly used variable amplitude multiaxial fatigue life analysis methods, including Bannantine-Socie method, Wang-Brown method and Wang L-Wang D J method are reviewed briefly based on the current researches on variable amplitude multiaxial fatigue. Then, the algorithms of the three methods we...

Maneuvering group target tracking with multi-model GGIW-GLMB algorithm
GAN Linhai, LIU Jinmang, WANG Gang, LI Song
2018, 44(10): 2185-2192. doi: 10.13700/j.bh.1001-5965.2018.0053
Abstract:

An multi-model Gamma Gaussian inverse Wishart-generalized labeled multi-Bernoulli (MM-GGIW-GLMB) algorithm is proposed for multiple maneuvering group target tracking. A multi-model approach is introduced for kinematic modeling, and best fitting Gauss (BFG) approximation is used to fuse the multiple ...

Exact background subtraction processing technique in RCS measurement in time-variant environment
YUAN Saisai, LIANG Liya, XU Xiaojian
2018, 44(10): 2193-2199. doi: 10.13700/j.bh.1001-5965.2018.0019
Abstract:

In outdoor radar cross section (RCS) measurement, background clutter cannot be suppressed effectively using conventional background subtraction technique due to the fact that, influenced by time-variant outdoor environment, the amplitudes and phases of radar received returns collected at different t...

Tether swing control of tethered system based on nonlinear model prediction
ZHANG Yujing, ZHONG Rui
2018, 44(10): 2200-2207. doi: 10.13700/j.bh.1001-5965.2017.0810
Abstract:

On the stability control of the rope system, a stability control method of tether swing for tethered system consisting of tether and tethered satellites during deorbitting is proposed in this paper. In this paper, a model of motion including satellite attitude motion is eatablished, and the dynamic ...

A 3D laser scanning system design and parameter calibration
CAI Jun, ZHAO Yuan, LI Yuhao, XIE Yangmin
2018, 44(10): 2208-2216. doi: 10.13700/j.bh.1001-5965.2018.0029
Abstract:

Dynamic environment map construction technology based on 3D laser scanning system has been served as one of the important intelligent perception technologies for mobile robots. The design and calibration of 3D laser scanning system place a decisive influence on the accuracy of the constructed enviro...

Inter-block physical layer security structure design for polar code under FTN transmission
ZHANG Chenyu, LIU Rongke
2018, 44(10): 2217-2223. doi: 10.13700/j.bh.1001-5965.2018.0007
Abstract:

Wiretap channel is a widely-used model to describe physical layer security and polar code shows potential in wiretap channel model due to its polarization characteristic. A new inter-block encryption security scheme without the need of acquiring signal-to-noise ratio (SNR) is designed for the polar ...

Numerical simulation of melting process of phase change energy storage unit under microgravity
RUAN Shiting, ZHANG Jimin, CAO Jianguang, WANG Jiang, XU Tao
2018, 44(10): 2224-2231. doi: 10.13700/j.bh.1001-5965.2017.0791
Abstract:

In order to explore the melting process of phase change materials in the phase change energy storage unit with fins in microgravity environment, the heat transfer and flow characteristics of phase change materials in microgravity environment are investigated by numerical simulation. The accuracy of ...

Measurement and extraction technique of scattered signals for targets under complex background
LIANG Liya, YUAN Saisai, XU Xiaojian
2018, 44(10): 2232-2237. doi: 10.13700/j.bh.1001-5965.2018.0020
Abstract:

Zero-Doppler clutter (ZDC) caused by the surrounding environment of an outdoor measurement field is one of the major factors which degrade the accuracy of the target scattering signatures in wideband radar cross section measurement. A new technique for ZDC estimation based on maximal probability is ...

Aero-engine working condition recognition based on MKSVDD optimized by improved BA
HE Dawei, PENG Jingbo, HU Jinhai, SONG Zhiping
2018, 44(10): 2238-2246. doi: 10.13700/j.bh.1001-5965.2017.0756
Abstract:

In order to ameliorate the accuracy and efficiency of aero-engine working condition identification, and to avoid the misjudgment and time-consuming problems in manual identification of aero-engine working condition, an intelligent recognition method, multi-kernel support vector data description base...