2023 Vol. 49, No. 8

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Volume 8 Issue E-journal
Volume 49 Issue82023
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Text-to-image synthesis based on modified deep convolutional generative adversarial network
LI Yunhong, ZHU Mianyun, REN Jie, SU Xueping, ZHOU Xiaoji, YU Huikang
2023, 49(8): 1875-1883. doi: 10.13700/j.bh.1001-5965.2021.0588
Abstract:

When high-dimensional texts are adopted as input,images generated by the previously proposed deep convolutional generative adversarial network (DCGAN) model usually suffer from distortions and structure degradation due to the sparsity of texts, which seriously poses a negative impact on the generati...

Detection of railway object intrusion under infrared low light based on multi-feature and attention enhancement network
CHEN Yong, WANG Zhen, LU Chentao, ZHANG Jiaojiao
2023, 49(8): 1884-1895. doi: 10.13700/j.bh.1001-5965.2021.0591
Abstract:

There are some problems in railway object intrusion detection in infrared weak light environment, such as insufficient target feature extraction, low detection accuracy and real-time performance. Aiming to those problems, an anchor-free object intrusion depth learning model based on CenterNet target...

Fault diagnosis of generator rolling bearing based on AE-BN
WANG Jinhua, GAO Yuan, CAO Jie, MA Jialin
2023, 49(8): 1896-1903. doi: 10.13700/j.bh.1001-5965.2021.0581
Abstract:

To solve the accuracy of fault identification of wind turbines under complex working conditions, coupling, and uncertainty, an AE-BN fault diagnosis method based on a auto-encoder (AE) and Bayesian network (BN) is proposed. AE is used to extract the characteristics of the current signal, and the cha...

Dynamic characteristics of turbine flowmeter based on CFD simulation
GUO Suna, SONG Wei, XIANG Nuolin, LIU Xu, WANG Fan, ZHAO Zhiyue
2023, 49(8): 1904-1911. doi: 10.13700/j.bh.1001-5965.2021.0594
Abstract:

Currently, the aerospace industry has increasingly strict requirements for flow measuring, and therefore, studying the dynamic characteristics of the flowmeter is of great significant for improving the measurement performance and online measurement performance in various environments. In this paper,...

Accuracy analysis of Eulerian method for droplet impingement characteristics under aircraft icing conditions
SHEN Xiaobin, ZHAO Wenzhao, LIN Guiping, QI Zicheng
2023, 49(8): 1912-1921. doi: 10.13700/j.bh.1001-5965.2021.0607
Abstract:

The calculation of super-cooled droplet impingement characteristics is the basis for the prediction of ice shape and the performance analysis of anti-icing and de-icing systems under icing conditions. Eulerian and Lagrangian methods are the commonly used ones, and their predictions are usually consi...

Calculation of cutting angle and cutting force in face gear machining
GUAN Rui, HUANG Yizhan, CHEN Rui, WANG Yanzhong
2023, 49(8): 1922-1929. doi: 10.13700/j.bh.1001-5965.2021.0613
Abstract:

Combining a method for skiving cylindrical gear with one for machining face gear is suggested in order to increase the processing effectiveness of face gears. First, the principle of the skiving machining is analyzed, and the machining motion model and the skiving coordinate system are established. ...

A safety analysis approach for embedded system
YANG Bo, LIU Zhen, WEI Xinjie, WU Ji
2023, 49(8): 1930-1939. doi: 10.13700/j.bh.1001-5965.2022.0185
Abstract:

Embedded systems are widely used in safety-critical industrial fields, but currently the safety of embedded systems lacks a comprehensive analysis. Therefore, a fault evolution chain analysis method for embedded systems has been proposed, which integrates failure probability and failure path. Firstl...

Unsteady flow mechanism of high Mach number cavity
ZHANG Peihong, CHENG Xiaohui, CHEN Hongyang, JIA Hongyin, LUO Lei, TANG Yin
2023, 49(8): 1940-1947. doi: 10.13700/j.bh.1001-5965.2021.0609
Abstract:

The cavity flow widely exists in aircraft, and the flow in embedded weapon bay is one of the most typical cavity flows. The cavity flow has a complex structure and generates strong pressure fluctuations due to the interaction of shear layers, vortices, and shock waves. Using the unstructured hybrid ...

Process control net modelling and analyzing for satellite test and evaluation in launch site
ZHANG Chun, ZHUANG Ke, YU Peng, YAN Jindong, LIU Yifan, CHANG Jin
2023, 49(8): 1948-1955. doi: 10.13700/j.bh.1001-5965.2021.0628
Abstract:

During the prelaunch phase, the process control combines test models with subjects to enable the design and modification of satellite test and evaluation procedures. Since non-structural words and images are mostly used to describe and build the technical process of the satellite at the launch site,...

Cooperative guidance method with interception time constraint
ZHANG Shuai, SONG Tianli, JIAO Wei, GUO Yang
2023, 49(8): 1956-1963. doi: 10.13700/j.bh.1001-5965.2021.0569
Abstract:

To address the problem of multi-aircraft cooperative interception of maneuvering targets, a cooperative guidance method considering interception time constraints is proposed based on the finite-time sliding mode control method and consistency theory. Based on the relative kinematics and dynamics, a ...

Aircraft landing safety quality analysis based on modified FRAM method
YAN Yifan, GAN Xusheng, WU Yarong, YANG Liwei
2023, 49(8): 1964-1973. doi: 10.13700/j.bh.1001-5965.2021.0574
Abstract:

The aircraft landing stage poses the highest risk of flight accidents and demands the most rigorous technical skills from pilots. Thus, a scientific assessment system should be established to accurately evaluate pilots’ technical skills of landing control, identify their technical defects, and formu...

Optimization of discharge chamber key parameters for 10 cm Kaufman xenon ion thruster
HU Jing, GENG Hai, YANG Fuquan, GUO Dezhou, WANG Dongsheng, LI Jianpeng
2023, 49(8): 1974-1981. doi: 10.13700/j.bh.1001-5965.2021.0631
Abstract:

Discharge chamber configuration is the foundation and core of ion thruster structure design, which directly influences the working efficiency of the discharge chamber and in-orbit lifetime of the thruster. Aiming at the application requirement of new complex aerospace equipment for ion thruster with...

Energy-efficiency characteristic investigation of rotational inertia hydraulic converter
CHEN Xiaoming, ZHU Yuchuan, LING Jie, ZHENG Shufeng, WANG Yuwen
2023, 49(8): 1982-1990. doi: 10.13700/j.bh.1001-5965.2021.0570
Abstract:

To explore the main characteristics and energy conversion mechanism of rotational inertia hydraulic converter (RIHC). Using a rotating inertia hydraulic converter configuration powered by an analogous rapid switching valve, the overall theoretical model was developed to investigate the key features ...

Residual SDE-Net for uncertainty estimates of deep neural networks
WANG Yongguang, YAO Shuzhen, TAN Huobin
2023, 49(8): 1991-2000. doi: 10.13700/j.bh.1001-5965.2021.0604
Abstract:

The neural stochastic differential equation model (SDE-Net) can quantify epistemic uncertainties of deep neural networks (DNNs) from the perspective of a dynamical system. However, SDE-Net faces two problems. Firstly, when dealing with largescale datasets, performance degrades as network layers incr...

A cooperative search and encirclement algorithm for quadrotors in unknown areas
GUO Jinjin, QI Juntong, WANG Mingming, WU Chong, XU Shibo
2023, 49(8): 2001-2010. doi: 10.13700/j.bh.1001-5965.2021.0606
Abstract:

Quadrotor swarms can be used for regional reconnaissance to establish the cognition of the environment and targets. This study offers a distributed cooperative search algorithm and a dynamic target surrounding technique for quadrotor swarm to solve the challenge of locating and monitoring targets in...

Interface adjustment of aerospace-grade T800 carbon fiber composite material
LI Tianshu, WANG Shaokai, WU Qing, GU Yizhuo, LI Qinghui, LI Min
2023, 49(8): 2011-2020. doi: 10.13700/j.bh.1001-5965.2021.0619
Abstract:

The effect of the sizing agent on the surface modification of high-performance carbon fiber (CF) and the modulation effect on the interface performance of its composite is very important. In this paper, the aerospace-grade T800 carbon fibers prepared by the wet method are used, and the changes in th...

Collapse modes and energy absorption performance of conventional and re-entrant hexagonal tubes under lateral compression
LIU Jie, LIU Hua, YANG Jialing
2023, 49(8): 2021-2028. doi: 10.13700/j.bh.1001-5965.2021.0623
Abstract:

Hexagonal thin-walled structures are widely used in the field of energy absorption and protection. To improve the energy absorption performance of hexagonal thin-walled tubes, in this study, a comparative study on the collapse modes and energy absorption performance of the conventional and re-entran...

Architecture of smart parking lot based on digital twin technology
SHANG Ke, ZHANG Yulin, ZHANG Feizhou
2023, 49(8): 2029-2038. doi: 10.13700/j.bh.1001-5965.2021.0624
Abstract:

In the research on the construction of large and medium-sized parking lots in cities, the current focus is mainly on hardware upgrades and simple human-computer interactions. However, neither the low use of big data nor the divergence between digital simulation and actual things has been resolved. B...

Strain-based geometrically nonlinear beam modeling and analysis
XU Qiuyi, MENG Yang, LI Shu
2023, 49(8): 2039-2049. doi: 10.13700/j.bh.1001-5965.2021.0627
Abstract:

Under the action of aerodynamic forces, flexible wings undergo large deformations, for which geometric nonlinearity cannot be ignored. By taking advantage of their slenderness, flexible wings can be modeled as beams. This paper developed the dynamic equilibrium equations of nonlinear beams based on ...

Safety helmet detection algorithm based on improved YOLOv5s
ZHAO Rui, LIU Hui, LIU Peilin, LEI Yin, LI Da
2023, 49(8): 2050-2061. doi: 10.13700/j.bh.1001-5965.2021.0595
Abstract:

A YOLOv5s-based helmet detection improvement method is developed in an effort to address the drawbacks of existing safety helmet recognition algorithms, which include difficulty detecting small targets and dense targets. The DenseBlock module is used to replace the slice structure in the backbone ne...

Altitude control of stratospheric aerostat based on deep reinforcement learning
ZHANG Jinglun, YANG Xixiang, DENG Xiaolong, GUO Zheng, ZHAI Jiaqi
2023, 49(8): 2062-2070. doi: 10.13700/j.bh.1001-5965.2021.0622
Abstract:

A dynamic model of the stratospheric aerostat was built with the goal of controlling the aerostat's altitude while taking air temperature into consideration, and a method based on the deep Q-network (DQN) algorithm was developed. Due to the difficulty in predicting the stratospheric wind field and t...

Point cloud registration algorithm for non-cooperative targets based on Hough transform
SHI Fengyuan, ZHENG Xunjiang, JIANG Lihui, PAN Di, LIU Xuan
2023, 49(8): 2071-2078. doi: 10.13700/j.bh.1001-5965.2021.0575
Abstract:

To solve the problems of missing and fast maneuvering non-cooperative space targets during the point cloud registration, this study examines the point cloud registration process of time-of-flight (TOF) cameras. It proposes a point cloud registration strategy based on Hough transform, utilizing the f...

Degradation-shock competing failure modeling considering randomness of failure threshold
XIA Yuexin, FANG Zhigeng
2023, 49(8): 2079-2088. doi: 10.13700/j.bh.1001-5965.2021.0576
Abstract:

Since most research on competing failure reliability do not take the unpredictability of the failure threshold into account, a competing failure reliability model that takes the randomness of the failure threshold into account is devised. The variation of degradation quantity and degradation rate un...

Automatic modulation recognition method based on improved weight AdaBoost.M2 algorithm
WANG Pei, LIU Chunhui, ZHANG Duona
2023, 49(8): 2089-2098. doi: 10.13700/j.bh.1001-5965.2021.0577
Abstract:

A signal modulation recognition method is proposed based on AdaBoost.M2 algorithm to address difficult identification of signals from the same family of modulation types and the poor generalization of the deep learning model. An improved method of sample weight is proposed to solve the problem that ...

Area optimization of FPRM logic circuits based on SMABC algorithm
QIN Dongge, HE Zhenxue, CHEN Chen, LI Longhao, WANG Tao, WANG Xiang
2023, 49(8): 2099-2107. doi: 10.13700/j.bh.1001-5965.2021.0579
Abstract:

The area optimization of fixed polarity Reed-Muller (FPRM) circuits is one of the most important research hotspots in the field of integrated circuit design. However, the existing area optimization methods have problems such as low optimization efficiency and poor optimization effect. Since the area...

Safety priority path planning method based on Safe-PPO algorithm
BIE Tong, ZHU Xiaoqing, FU Yu, LI Xiaoli, RUAN Xiaogang, WANG Quanmin
2023, 49(8): 2108-2118. doi: 10.13700/j.bh.1001-5965.2021.0580
Abstract:

The existing path planning algorithms seldom consider the problem of security, and the traditional proximal policy optimization(PPO) algorithm has a variance adaptability problem. To solve these problems, the Safe-PPO algorithm combining evolutionary strategy and safety reward function was proposed....

Application of kernel principal component analysis in autonomous fault diagnosis for spacecraft flywheel
NIE Xiaohui, JIN Lei
2023, 49(8): 2119-2128. doi: 10.13700/j.bh.1001-5965.2021.0582
Abstract:

Aiming at the problems of relatively few studies on actuator fault diagnosis of on orbit spacecraft, relatively simple background modeling for attitude control system and weak algorithm autonomy, an autonomous fault diagnosis method for spacecraft flywheel based on kernel principal component analysi...

Modeling method of flight test requirements based on DoDAF
LIU Sen, YANG Dezhen, FENG Qiang, REN Yi, DANG Huaiyi, JIA Yu
2023, 49(8): 2129-2136. doi: 10.13700/j.bh.1001-5965.2021.0584
Abstract:

The flight test is a scientific, practical, dangerous, and complex process, and the current method of determining flight test requirements based on experience is rather unscientific. Combined with the characteristics of flight tests and based on DoD architectural framework 2.0, this paper proposes a...

UAV formation control based on dueling double DQN
ZHAO Qi, ZHEN Ziyang, GONG Huajun, CAO Hongbo, LI Rong, LIU Jicheng
2023, 49(8): 2137-2146. doi: 10.13700/j.bh.1001-5965.2021.0601
Abstract:

To address issues such as the need for controller design based on model information in UAV formation and the low level of UVA intelligence, deep reinforcement learning is used to solve formation control problems. In this paper, the corresponding reinforcement learning elements are designed for the f...

Study on temperature control characteristics of low-resistivity ceramic-based PTC material
SANG Zekang, ZHAO Rui, CHENG Wenlong
2023, 49(8): 2147-2153. doi: 10.13700/j.bh.1001-5965.2021.0602
Abstract:

The room temperature Curie point ceramic-based positive temperature coefficient material has broad application prospects in the field of thermal control at room temperature, but it currently has the problem of large resistivity in the low-temperature region. Based on this, by using Ba0.64Sr0.36TiO3 ...

Gait based cross-view pedestrian tracking with camera network
SONG Shujie, WAN Jiuqing
2023, 49(8): 2154-2166. doi: 10.13700/j.bh.1001-5965.2021.0610
Abstract:

Pedestrian tracking across non-overlapping camera views is one of the basic problems of intelligent visual surveillance. A cross-view pedestrian target tracking method based on the gait features of a 2D skeleton diagram and space-time constraints is proposed in order to address the issue that the pe...

A real-time correlation algorithm for GEO targets based on radar ranging and velocity measurement
SONG Liping, CHEN Defeng, TIAN Tian, GUO Xin
2023, 49(8): 2167-2175. doi: 10.13700/j.bh.1001-5965.2021.0615
Abstract:

In order to address the issue of error correction of the geosynchronous orbit (GEO) targets under the dense track, a real-time correlation algorithm for the GEO targets based on the two-dimensional of radar range and velocity measurement was developed. Firstly, the initial target set is established ...

Dual-input dual-Buck aviation static inverter with four-quadrant operation and circulation-free
YU Zhaolong, GE Hongjuan, WANG Yongshuai, YIN Hang, LI Shizhen
2023, 49(8): 2176-2186. doi: 10.13700/j.bh.1001-5965.2021.0625
Abstract:

The aviation static inverter (ASI) is a key part of the airborne power system, and inorder to further improve the efficiency and reliability of the ASI, an efficient and Ihighly reliable circulation-free ASI topology is proposed on the basis of thedual-input dual-Buck inverter technology. The topolo...

Improvement and application of hybrid strategy-based sparrow search algorithm
SONG Liqin, CHEN Wenjie, CHEN Weihai, LIN Yan, SUN Xiantao
2023, 49(8): 2187-2199. doi: 10.13700/j.bh.1001-5965.2021.0629
Abstract:

Aiming at solving the problems in the original sparrow search algorithm (SSA), such as low search accuracy, weak global search ability, slow convergence speed and easy tendency to fall into local optimum, a hybrid strategy-based sparrow search algorithm (HSSA) is proposed. First, an improved Circle ...

Corrosion and fatigue life prediction of aircraft typical lap structures based on life envelope
BI Yaping, ZHANG Teng, HE Yuting, ZHANG Tianyu, WANG Changkai
2023, 49(8): 2200-2206. doi: 10.13700/j.bh.1001-5965.2022.0604
Abstract:

The corrosion and fatigue tests of a certain type of aircraft fuselage panel lap structure were conducted alternatively. Based on the test results and the concept of aircraft structure life envelope, the life envelope of the lap joint structure of the fuselage panel in different service areas and un...