2023 Vol. 49, No. 7

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Volume 7 Issue E-journal
Volume 49 Issue72023
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Conception and development of software-defined satellite technology
XU Fanjiang, ZHOU Xin, ZHAO Junsuo, WU Fengge, LIN Yijun, XIA Yuli
2023, 49(7): 1543-1552. doi: 10.13700/j.bh.1001-5965.2021.0562
Abstract:

Focusing on the trend of massive, networked, and intelligent development of in-orbit satellites, this paper explores the background, concept, and trends of software-defined satellite technology as well as the challenges it is faced today. First, it is presented that the satellite system is evolving ...

Experimental study on adverse attitude emergency evacuation of civil aircraft after crash landing
FENG Wenchun, ZHANG Tong, LI Wei
2023, 49(7): 1553-1562. doi: 10.13700/j.bh.1001-5965.2021.0483
Abstract:

Based on dynamic emergency evacuation test environment, the effects of adverse attitude on emergency evacuation were studied and more than two hundred tests, including individual evacuation and group evacuation tests, were implemented. Then the average evacuation speed of individuals at seat and ais...

Improved PSO-RBF neural network adaptive sliding mode control for quadrotor systems
TANG Zhiyong, MA Fuyuan, PEI Zhongcai
2023, 49(7): 1563-1572. doi: 10.13700/j.bh.1001-5965.2021.0477
Abstract:

An improved particle swarm optimization-radial basis function (PSO-RBF) neural network adaptive sliding mode controller is proposed for quadrotor systems with nonlinearity, strong coupling, and inaccurate interference. First, based on smooth improvement of the control amount of the RBF neural networ...

Design and experiment of cryogenic loop heat pipe of two-dimensional pointing at liquid nitrogen zone
LI Nan, GUO Yuandong, XU Cheng, ZHANG Hongxing, LIN Guiping
2023, 49(7): 1573-1582. doi: 10.13700/j.bh.1001-5965.2021.0500
Abstract:

The cooperation of the two-dimensional pointing mechanism and the infrared detector is conducive to the realization of large-scale dynamic tracking, pointing, and rapid positioning of space targets. Coupling the cryogenic loop heat pipe (CLHP) with the two-dimensional pointing mechanism can greatly ...

Sensor fault detection and data reconstruction method of power supply vehicle
JIANG Dongnian, BA Yujiang, LI Wei
2023, 49(7): 1583-1592. doi: 10.13700/j.bh.1001-5965.2021.0501
Abstract:

Aiming at the problem that the power supply vehicle is prone to sensor fault due to the complex operating environment, a sensor fault detection and data reconstruction method based on spatiotemporal correlation is proposed in this paper. Firstly, according to the time-series relationship characteris...

Segmentation extraction of feature points for time series pattern matching
LI Zhengxin, LIU Chang, WU Shihui, GUO Jiansheng
2023, 49(7): 1593-1599. doi: 10.13700/j.bh.1001-5965.2021.0546
Abstract:

It is difficult for the common time series pattern matching methods to balance the computational complexity and matching accuracy. To solve this problem, a time series matching method based on segmented extraction of feature points is proposed. Firstly, the feature points on each variable dimension ...

Precise orbit determination method for angle-only observation data of space debris based on angle conversion theory
ZHANG Yao, LIU Jing
2023, 49(7): 1600-1605. doi: 10.13700/j.bh.1001-5965.2021.0507
Abstract:

On the basis of the angle conversion method, a brand-new accurate orbit determination technique for space debris was developed. First, based on the commonly used two-line-element (TLE) data application requirements, a TLE precise orbit determination model based on the SGP4/SDP4 forecast model was es...

Secondary electron multiplication of aluminum under strong vacuum electromagnetic field
SHANG Shengfei, YANG Xiaoning, YANG Yong, BI Yanqiang, WU Nankai, YU Lantao
2023, 49(7): 1606-1613. doi: 10.13700/j.bh.1001-5965.2021.0514
Abstract:

This paper primarily employs the 1D3V particle-in-cell (PIC) method to investigate the rule of multifactor of aluminum material on satellite surface under the strong electromagnetic environment of space in order to study the charge and discharge effect brought on by the strong electromagnetic enviro...

Tensile fatigue properties of carbon fiber laminates in hygrothermal environments
XU Mingrui, ZENG Benyin, XIONG Xin, MENG Qingchun, CHENG Xiaoquan
2023, 49(7): 1614-1622. doi: 10.13700/j.bh.1001-5965.2021.0565
Abstract:

The hygrothermal environment is one of the main factors affecting the mechanical properties of composite laminates. To maintain the safety of the flight structures, it is crucial to study how hygrothermal conditions affect composite structures.The tensile fatigue properties of carbon fiber composite...

A sparse estimation method for radar target direction with sliding-window subarray configuration in mainlobe jamming
ZHOU Bilei, LI Rongfeng, ZENG Li, CHEN Hui, LIU Weijian, LI Binbin
2023, 49(7): 1623-1629. doi: 10.13700/j.bh.1001-5965.2021.0552
Abstract:

The suppression of mainlobe jamming (MLJ) is a hard task and an open problem in the radar field. This paper considers the problem of radar target direction estimation in MLJ. Hence, we propose a sparse estimation method for radar target direction with sliding-window subarray configuration in MLJ. ML...

Configuration and multibody separation scheme of compact missile swarm
FU Jiawei, WANG Chen
2023, 49(7): 1630-1638. doi: 10.13700/j.bh.1001-5965.2021.0508
Abstract:

One type of missile swarm system is proposed, where numerous small UAVs are compressed in a missile carrier, to solve the weakness of swarm penetration capability and operational radius while speeding up the formation of cooperation. It uses tactics by multistage transport, making the swarm deploy r...

Multi-objective optimization of aerodynamic layout for hypersonic reentry vehicle
FAN Boxuan, CHEN Guiming, CAO Yiqun
2023, 49(7): 1639-1650. doi: 10.13700/j.bh.1001-5965.2021.0566
Abstract:

Multi-objective optimization of aerodynamic layout is a key technology in aircraft design. A new multi-objective optimization method is proposed for aerodynamic shape parameters of hypersonic reentry vehicle, and then the influence of the method on the performance of hypersonic reentry vehicle is pr...

Mechanism of butterfly forward flight and prototype verification based on characteristic motion observation
ZHANG Yixin, WANG Xingjian, WANG Shaoping, CHI Xiaokai, DU Shaoyang
2023, 49(7): 1651-1660. doi: 10.13700/j.bh.1001-5965.2021.0497
Abstract:

To investigate the mechanism of butterfly flapping wing flight and develop a low-frequency flapping wing bionic robot, the fligh kinematics of the butterfly are capturedand documented using a high-speed camera, three characteristic motion states of butterflies are proposed: flapping wing motion, tho...

Soil moisture retrieval using Beidou GEO satellite interference signal power
HAN Mutian, XU Zhichao, CHANG Qing, ZHANG Bo, WANG Feng, HONG Xuebao
2023, 49(7): 1661-1670. doi: 10.13700/j.bh.1001-5965.2021.0478
Abstract:

Soil moisture retrieval using Beidou geostationary Earth orbit (GEO) interference signal power was studied. Current researches mainly establish empirical models for retrieving soil moisture. Therefore, a semi-empirical retrieval method was proposed. Taking the advantage of Beidou GEO satellite’s sta...

Aerodynamic performance analysis of supercritical airfoil with lower surface jet
WANG Ruochen, ZHANG Guoxin, WANG Xiangyu, MA Xiaoping
2023, 49(7): 1671-1679. doi: 10.13700/j.bh.1001-5965.2021.0489
Abstract:

To investigate the influence of key parameters of the lower surface jet on aerodynamic performance of supercritical airfoil, a numerical simulation is performed using Reynolds average Navier-Stokes (RANS) equation and Spalart-Allmaras (S-A) turbulence model. By comparing the flow field between the b...

Numerical study of blood pump weaning effects on hemocompatibility of centrifugal blood pump
XIE Nan, TANG Yumeng, ZHANG Yan, LIU Yangwei
2023, 49(7): 1680-1688. doi: 10.13700/j.bh.1001-5965.2021.0494
Abstract:

The four stages of blood pump weaning are used to methodically assess the hemodynamic performance and hemocompatibility of the datum and modified centrifugal blood pumps. The distribution of parameters and the changes of normalized index of hemolysis in four stages of weaning are researched, the pre...

Aerodynamic order reduction method for elastic aircraft flight dynamics simulation
SHI Yan, WAN Zhiqiang, WU Zhigang, GONG Yinan
2023, 49(7): 1689-1706. doi: 10.13700/j.bh.1001-5965.2021.0510
Abstract:

We develop an aeroelasticity and flight dynamics simulation model with nonlinear aerodynamic reduced order model for low-speed solar unmanned aerial vehicles under high angle of attack caused by gust. Five aerodynamic reduced-order models are created in light of the aforementioned issues, and their ...

Experiment research on high-speed ultrasonic vibration milling of titanium alloy
HAN Xiong, SUN Zhefei, GENG Daxi, ZHANG Deyuan
2023, 49(7): 1707-1714. doi: 10.13700/j.bh.1001-5965.2021.0519
Abstract:

Conventional milling (CM) causes problems for titanium alloys, such as high cutting forces, large deformation of thin-walled workpieces, low processing efficiency, and severe tool wear due to low cutting speeds. To address these problems, a new method of high-speed ultrasonic vibration milling (HUVM...

Simulation analysis of reduction effect of symmetrical winding method for multi-polar fiber ring on Shupe error
ZHANG Dongbo, WANG Lixin, LI Can
2023, 49(7): 1715-1721. doi: 10.13700/j.bh.1001-5965.2021.0530
Abstract:

The Shupe bias error is one of the biggest bottleneck problems in the engineering application of interferometric fiber optic gyroscope (IFOG). A turn-by-turn finite element model for fiber coils is established in this article. Based on this model, analyze the temperature performance of the 8 level, ...

Design and performance analysis of spatial large extension parallel mechanism
HE Litao, FANG Hairong, CHEN Yufei, LI Yin
2023, 49(7): 1722-1734. doi: 10.13700/j.bh.1001-5965.2021.0548
Abstract:

In the process of large-scale workpiece machining, the insufficient extension space of the executive mechanism is an urgent problem to be solved in the aerospace manufacturing industry. To increase the working space at the end of the executive mechanism, and to provide the mechanism with a stable an...

Analysis of influence of ultrasonic drilling structure parameters on output characteristics
ZHANG Xingwang, ZHANG Ming, YU Dengyun, ZENG Ting, YIN Shen, YANG Shuai, PANG Yong
2023, 49(7): 1735-1742. doi: 10.13700/j.bh.1001-5965.2021.0554
Abstract:

The ultrasonic drill has the characteristics of lightweight, low power consumption, the small axial force required, easy real-time detection and in-situ analysis, and good adaptability to different objects. It is highly anticipated in exploring new scientific drilling technologies and new methods su...

Pedestrian trajectory prediction method based on pedestrian pose
WANG Ruiping, SONG Xiao, CHEN Kai, GONG Kaiqi, ZHANG Junfan
2023, 49(7): 1743-1754. doi: 10.13700/j.bh.1001-5965.2021.0557
Abstract:

In the field of autonomous driving, pedestrian trajectory prediction has been one of the research hotspots, and the uncertainty of pedestrian behavior poses a great challenge to trajectory prediction. Most of the current trajectory prediction methods only focus on the information interaction between...

Improved modeling strategy and result evaluation of steroid-induced femoral head necrosis in rabbits
YANG Fenghe, FENG Guiyu, LI Jinyu, NIU Xufeng
2023, 49(7): 1755-1760. doi: 10.13700/j.bh.1001-5965.2021.0558
Abstract:

The establishment of animal model of femoral head necrosis is of great significance for the clinical treatment of this disease. To successfully induce femoral head necrosis while reducing the mortality of modeling animals, this study improves the commonly used modeling method of steroid-induced femo...

Influence of rotor/wing aerodynamic interference on performance of compound helicopters
YANG Kelong, HAN Dong
2023, 49(7): 1761-1771. doi: 10.13700/j.bh.1001-5965.2021.0561
Abstract:

To investigate the influence of rotor/wing aerodynamic interference on the high-speed flight performance of a dual-propeller propelled compound helicopter, a flight performance prediction model of compound helicopters is established. Taking the AS365N ‘Dolphin’ helicopter equipped with a wing and pr...

Weakly supervised evaluation of airport traffic situation based on metric learning
DU Jinghan, HU Minghua, ZHANG Weining, YIN Jianan
2023, 49(7): 1772-1778. doi: 10.13700/j.bh.1001-5965.2021.0568
Abstract:

In order to accurately perceive the operating environment of the airport surface, a weakly supervised evaluation method of traffic situation based on metric learning is proposed. Firstly, according to the space-time distribution types of aircraft on the airport surface, the traffic situation index s...

Influence of open water in retrieval of soil moisture by spaceborne GNSS-R
YANG Wentao, XU Tianhe, WANG Nazi, GAO Fan, JING Lili, HE Yunqiao
2023, 49(7): 1779-1786. doi: 10.13700/j.bh.1001-5965.2021.0479
Abstract:

Soil moisture(SM) information can be obtained through the high spatial and temporal resolution spaceborne GNSS-R technology, however, open water will affect the accuracy of the retrieval results. To solve this problem, this paper proposes an improved method of removing open water. Prior to precisely...

UAV information interaction topology generation considering task allocation
XUE Ying, HE Feng, GU Xiaoyan
2023, 49(7): 1787-1795. doi: 10.13700/j.bh.1001-5965.2021.0486
Abstract:

The optimization of information interaction topology for persistent unmanned aerial vehicle (UAV) formation is an important basis for the stability of UAV formation structure and the timeliness of task execution. The existing formation generation algorithms assign weights and generate topologies bas...

Design of robust controller for single outrigger of vibration active isolation platform based on LPV
TANG Yucong, ZHU Qinghua, LIU Fucheng, CAO Heyang
2023, 49(7): 1796-1801. doi: 10.13700/j.bh.1001-5965.2021.0513
Abstract:

When the control moment gyro (CMG) is used to achieve agile attitude maneuvering control, the mechanical CMG vibration should be effectively isolated after the maneuvering is in place to achieve high-stability attitude control, while the rapid response of the control output torque is ensured during ...

Double-loop surrogate model for time-dependent reliability analysis based on NARX and Kriging models
CHANG Zeming, LI Luyi
2023, 49(7): 1802-1812. doi: 10.13700/j.bh.1001-5965.2021.0541
Abstract:

Structural systems with dynamic output performance has gained more and more attention in engineering practice. However, most existing surrogate models for estimating time-dependent reliability of such systems only consider the effect of the random variables which are acting on the system at the curr...

Conflict resolution algorithms for UAV low-altitude flight based on reachable set
YANG Jianhang, ZHANG Fubiao, WANG Jiang
2023, 49(7): 1813-1827. doi: 10.13700/j.bh.1001-5965.2021.0542
Abstract:

Aiming at the conflict resolution problem in unmanned air traffic management (UTM), real-time collision avoidance algorithms based on reachability set analysis are proposed. To assure the secure operation of unmanned aerial vehicles (UAV) in low-altitude urban environments with dense traffic flow, t...

Semantic segmentation of remote sensing images based on U-shaped network combined with spatial enhance attention
BAO Yintu, LIU Wei, LI Runsheng, LI Qin, HU Qing
2023, 49(7): 1828-1837. doi: 10.13700/j.bh.1001-5965.2021.0544
Abstract:

The performance of semantic segmentation based on deep learning still need to be improved when analyzing small-sized objects and object boundaries in remote sensing images. Aiming at this problem, we propose a U-shaped network (SGE-Unet). Firstly, the structure of the model is optimized to enhance t...

Stacking scheduling method for time-triggered messages in off-chip network
ZANG Guangjie, LI Qiao, WANG Tong, XIONG Huagang
2023, 49(7): 1838-1846. doi: 10.13700/j.bh.1001-5965.2021.0553
Abstract:

To ensure the strict time determinism of message transmission between avionics communication tasks, time-triggered (TT) communication methods are also applied to the off-chip interconnection network. When avionics tasks have multiple operation modes, the time-triggered schedules between chips belong...

Detection of debonding defect in CFRP laminates using infrared pulse thermal wave tomography
ZHONG Jiacen, XU Haojun, WEI Xiaolong, HAN Xinmin, CHANG Yipeng
2023, 49(7): 1847-1856. doi: 10.13700/j.bh.1001-5965.2021.0555
Abstract:

To achieve the three-dimensional tomography for detecting debonding defects of carbon fiber reinforced plastic (CFRP) laminates based on infrared pulse thermal wave imaging, consummate the out-field quantitative detection guarantee system, and improve the safety and reliability of laminates in servi...

Uniform circular multiphase modulation correlation radiometer and its sensitivity analysis
CHEN Ruihou, LUO Jing, HU Anyong, MIAO Jungang
2023, 49(7): 1857-1863. doi: 10.13700/j.bh.1001-5965.2021.0560
Abstract:

A correlation radiometer structure with uniform multiphase modulation around the circumference is proposed in order to address the issue of decreased measurement accuracy caused by the operational amplifier’s offset drift and gain fluctuation in correlation radiometers. The measurement result is pro...

Numerical study of wing gust response alleviation based on camber morphing trailing edge
WEI Rukai, DAI Yuting, YANG Chao, YU Siheng
2023, 49(7): 1864-1874. doi: 10.13700/j.bh.1001-5965.2021.0563
Abstract:

A mathematical model for gust response analysis is established for a wing with camber morphing trailing edges, and a simulation study of gust response alleviation is carried out. The computational fluid dynamics method is used to calculate the generalized unsteady aerodynamic force under the given d...