2023 Vol. 49, No. 9

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Volume 9 Issue E-journal
Volume 49 Issue92023
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Non-standard interface aviation RF cable test method based on TRL
SHI Xudong, LI Ruipu, ZHAO Hongxu, ZHANG Haotian
2023, 49(9): 2207-2217. doi: 10.13700/j.bh.1001-5965.2021.0645
Abstract:

Aircraft radio frequency (RF) cables are the main medium for transmitting signals. There are currently various non-standard interface cables, and in order to use standard interface instruments for performance testing, precise adapter leads are required. However, the precise adapter leads have high r...

Robust optimization of aviation logistics network in context of COVID-19 pandamic
ZHANG Jin, ZHANG Zherui, HONG Zhichao, YANG Wenguang, YAN Yan
2023, 49(9): 2218-2226. doi: 10.13700/j.bh.1001-5965.2021.0664
Abstract:

To deal with the risk of reducing the capacity of passenger aircraft bellies due to the interruption of passenger aircraft routes in the context of COVID-19 pandemic, and to improve the robustness of the aviation logistics network at a minimum cost, a study on the allocation and route optimization o...

Rapid detection analysis method of thermal runaway gas composition and risk of lithium ion battery
ZHANG Qingsong, LIU Tiantian, HAO Chaolong, QU Yirun, ZHANG Wei, CHEN Da
2023, 49(9): 2227-2233. doi: 10.13700/j.bh.1001-5965.2021.0668
Abstract:

In order to quickly analyze the composition and risk of thermal runaway gas in lithium ion batteries, an analysis method based on laser Raman spectroscopy and the empirical formula is proposed. Using the independently designed gas detection platform of the lithium ion battery, the composition and ex...

Causal analysis framework of flight service
XING Zhiwei, ZHANG Lin, LUO Qian, XIA Huan, WEN Tao, ZHANG Tao
2023, 49(9): 2234-2243. doi: 10.13700/j.bh.1001-5965.2021.0679
Abstract:

Flight departure delay is a key and difficult problem that the civil aviation industry is unanimously concerned about. Aiming at the problem of unclear reasons for flight delays, the BLCNS-LV-IDA causality analysis framework is proposed. In the discipline of flight ground support business, causal an...

Target tracking algorithm based on saliency awareness and consistency constraint
GUO Qiang, WU Tianhao, XU Wei, CHORNOGOR Leonid
2023, 49(9): 2244-2257. doi: 10.13700/j.bh.1001-5965.2021.0688
Abstract:

Aimed at the problems that the spatially regularized discriminative correlation filtering (SRDCF) algorithm with fixed regularization weight and model degradation, a correlation filtering tracking algorithm based on saliency awareness and consistency constraint was proposed. Firstly, the histogram o...

Discharge model of divergent magnetic field ion thruster of 10 cm diameter
SUN Mingming, GENG Hai, HU Jing, YANG Fuquan, LONG Jianfei
2023, 49(9): 2258-2266. doi: 10.13700/j.bh.1001-5965.2021.0648
Abstract:

A discharge model of the divergent magnetic field ion thruster (Kaufman thruster) of 10 cm diameter is established with COMSOL multi-physical field coupling software to study the internal discharge process of the thruster and to provide reference for subsequent engineering improvement. The key disch...

Effect of engine nacelle layout on sonic boom of supersonic transport
XIAO Tianhang, XU Yanan, ZHU Zhenhao, DENG Shuanghou
2023, 49(9): 2267-2278. doi: 10.13700/j.bh.1001-5965.2021.0687
Abstract:

The strong aerodynamic interaction between the nacelles and the wing-body at supersonic speed, and the effect of the exhaust plume on the mainstream shock wave structure could have a great influence on the sonic boom loudness. This paper carries out a numerical investigation on the effect of nacelle...

Using improved genetic algorithm for software fault localization aided test case generation
YANG Bo, HE Yuze, XU Fu, CHEN Zhibo
2023, 49(9): 2279-2288. doi: 10.13700/j.bh.1001-5965.2022.0524
Abstract:

The ranking of suspected faults in the process of automatic software fault localization will be continuously created and is determined after the execution of existing test cases. Sometimes the program units corresponding to the fault are ranked lower in the ranking of suspected failures based on the...

Design of message authentication based on TESLA protocol for BDSBAS
CHEN Xiao, TIAN Xiang, LUO Ruidan, LIU Ting, SONG Jiahui, WU Haitao
2023, 49(9): 2289-2298. doi: 10.13700/j.bh.1001-5965.2021.0669
Abstract:

Aviation, navigation, and other life safety areas can benefit from the integrity augmentation services offered by SBAS. In response to the deception risk of SBAS services and the development of the BeiDou satellite-based augmentation system (BDSBAS), this paper proposes a message authentication meth...

Hydroplaning risk of aircraft tire based on variable weight theory-normal cloud model
LI Yue, HU Yuqi, CAI Jing, DAI Xuan
2023, 49(9): 2299-2305. doi: 10.13700/j.bh.1001-5965.2021.0680
Abstract:

Aiming at the randomness and fuzziness features of hydroplaning behavior of aircraft tires, a new safety evaluation methodology of tire hydroplaning is established on the basis of normal cloud model. The variable weight theory is adopted in order to adjust the weight value dynamically. The penalty f...

Simulation evaluation and analysis of aircraft group support based on multi-agent
DING Gang, CUI Lijie, HAN Cheng, WANG Xinhe, ZHANG Feng
2023, 49(9): 2306-2316. doi: 10.13700/j.bh.1001-5965.2021.0685
Abstract:

Aircraft group support involves a wide range of elements, multiple strategies, and strong interaction. Its simulation analysis method is a hot and difficult point in conducting research on aircraft group support decision-making and evaluation. This paper first establishes the multi-agent function ty...

Infrared and visible image fusion based on GEMD and improved PCNN
YANG Yanchun, LI Xiaomiao, DANG Jianwu, WANG Yangping
2023, 49(9): 2317-2329. doi: 10.13700/j.bh.1001-5965.2022.0756
Abstract:

Because of the limitations of decomposition tools in traditional image fusion methods, artifacts, decreased brightness, and contrast appear on fused image edges. A gradient edge-preserving multi-level decomposition(GEMD)-based approach for infrared and visible image fusion, as well as an enhanced pu...

Non-probabilistic reliability analysis method for propellent tank with crack defect
XIN Tengda, CUI Cunyan, LIU Yang, TONG Jiang, DUAN Yongsheng
2023, 49(9): 2330-2336. doi: 10.13700/j.bh.1001-5965.2021.0651
Abstract:

During the service period of the propellant tank, the accurate analysis of its crack defects and reliable state with crack defects can not only guarantee the safety of the launch site, but also effectively avoid unnecessary panic, providing a reference for emergency plan formulation. Based on interv...

Stability characteristics of hybrid wing-body aircraft based on virtual flight
WANG Yanling, FENG Shuai, BU Chen, SHEN Yanjie, CHEN Hao, LU Shiguang
2023, 49(9): 2337-2344. doi: 10.13700/j.bh.1001-5965.2021.0684
Abstract:

A three-degree-of-freedom wind tunnel virtual flight test system was created in an effort to address the possible stability issues of three-axis kinematic coupling and high angle-of-attack instability presented by the hybrid wing-body aircraft. Based on the dynamic similarity model, longitudinal and...

Error analysis and suppression of probe system for SERF atomic spin co-magnetometer
XING Li, QUAN Wei, SONG Tianxiao, CAI Qingzhong, YE Wen
2023, 49(9): 2345-2350. doi: 10.13700/j.bh.1001-5965.2021.0691
Abstract:

The performance of the probe system is the key factor to determine the sensitivity and stability limit of the spin-exchange relaxation-free (SERF) atomic spin co-magnetometer for inertial measurement. In order to suppress the low-frequency random noise in SERF auto spin co-magnetometer, the error me...

Extension method of engine low speed characteristics based on backbone features
WANG Jiamei, GUO Yingqing, YU Huafeng
2023, 49(9): 2351-2360. doi: 10.13700/j.bh.1001-5965.2021.0634
Abstract:

The blowing action of the incoming flow may cause the functioning state of the rotating components to alter when they operate at high altitudes but low speeds. The compressor is in a special “mixer” or “turbine” working state at such a condition, which makes a discontinuous change of efficiency duri...

Nonlinear flutter modes and flutter suppression of an all-movable fin with freeplay
BAI Liuyue, WU Zhigang, YANG Chao
2023, 49(9): 2361-2373. doi: 10.13700/j.bh.1001-5965.2022.0162
Abstract:

Freeplay nonlinearity widely exists in the structure of aircraft, which can bring limit cycle oscillations (LCO), leading to the fatigue failure of the structure. There is relatively little research on the mechanism and passive suppression of the nonlinear flutter for all-movable fins. Therefore, th...

Analyzing and modeling flow in tip clearance of transonic turbine rotor
XUAN Liming, ZOU Zhengping, ZENG Fei
2023, 49(9): 2374-2384. doi: 10.13700/j.bh.1001-5965.2021.0635
Abstract:

In order to clarify the mechanism of the tip leakage flow in transonic turbines and further improve turbine efficiency, the effect of tip injection on the performance of a flat tip and a squealer tip is studied under the transonic condition, and the flow state in the clearance between a flat tip and...

Vibration response of asphalt concrete pavement under vehicle-road coupled load
DONG Qian, CHENG Shaofeng, ZHANG Xianmin, BAO Yiting
2023, 49(9): 2385-2394. doi: 10.13700/j.bh.1001-5965.2021.0654
Abstract:

To study the vibration characteristics of asphalt concrete pavement, the time domain model of road roughness was simulated by the white noise filtering method, the coupling effect of vehicle and road with different vehicle speeds and different road roughness levels was analyzed based on the quarter ...

Adaptive fault diagnosis and estimation for quadrotor UAV
WANG Lina, LIU Zhenbao, YUAN Jinbiao, DANG Qingqing, JIANG Feihong, WANG Baodong
2023, 49(9): 2395-2405. doi: 10.13700/j.bh.1001-5965.2021.0656
Abstract:

A fault detection and estimation(FDA) method based on adaptive technology and observer is designed for common actuator faults of quadrotor unmanned aerial vehicle. In the stage of fault detection, the nonlinear diagnostic observer is designed, and the threshold value is derived by analytic function ...

Design and implementation of robot-assisted subretinal injection system
WANG Zhaodong, GUANG Chenhan, WANG Liqiang, ZONG Junjie, ZHENG Yu, YANG Yang
2023, 49(9): 2406-2414. doi: 10.13700/j.bh.1001-5965.2021.0667
Abstract:

Subretinal injection of human embryonic stem cells is an effective procedure for treating retinal degeneration, which imposes high demands on the precision, stability, and safety of the surgical procedure. To address these challenges, a robot-assisted retinal surgery system based on a master-slave c...

Trade-off for top-level requirements of commercial aircraft using comprehensive evaluation and optimization
FAN Zhouwei, YU Xiongqing, DAI Yalin
2023, 49(9): 2415-2422. doi: 10.13700/j.bh.1001-5965.2021.0670
Abstract:

As the key process of aircraft design, top-level requirements should be carefully considered at the beginning of design activities. A quantitative trade-off method for top-level requirements of commercial aircraft has been proposed. According to the relationship between top-level requirements and ai...

Design optimization of tow-steered composite structure targeting on manufacturing cost
CHEN Shize, LI Daochun, XIANG Jinwu
2023, 49(9): 2423-2431. doi: 10.13700/j.bh.1001-5965.2021.0677
Abstract:

Due to a number of limitations, traditional composite structure design approaches are unable to completely use the design space of composite. The realization of tow-steered composite brings new opportunities for improvement of the performance of composites. In this research, a tow-steered composite ...

Adjoint-based adaptive Cartesian mesh refinement for sonic boom prediction
ZHU Zhenhao, XIAO Tianhang, XU Yanan, DENG Shuanghou, ZHANG Zhenming, YU Xiongqing
2023, 49(9): 2432-2441. doi: 10.13700/j.bh.1001-5965.2021.0689
Abstract:

In view of the sonic boom prediction for supersonic transport, this paper develops a numerical method for supersonic near-field based on a finite volume scheme and an adjoint-based Cartesian adaptive mesh refinement for the governing equations. By solving the adjoint equation on an embedded-boundary...

Anti-occlusion target tracking algorithm of UAV based on multiple detection
ZHANG Boheng, CHAI Dongdong, MENG Lingbo, SUN Mingjian
2023, 49(9): 2442-2454. doi: 10.13700/j.bh.1001-5965.2021.0693
Abstract:

In this research, a multi-detection anti-occlusion target tracking method is suggested to address the issue of poor tracking effect when unmanned aerial vehicle (UAV) targets are occluded by obstacles during the target tracking process. A response confidence discrimination method is designed by fusi...

Regional classification of CO2 emission reduction potential of China’s civil aircraft
ZENG Wen, HU Rong, SONG Wen, LIU Zhihao, ZHANG Junfeng
2023, 49(9): 2455-2462. doi: 10.13700/j.bh.1001-5965.2021.0647
Abstract:

Scientific regional classification is fundamental for investigating aircraft CO2 emissions with regional differences and spatial relativity, and for proposing differentiated CO2 emission reduction measures. Using aircraft operation data from China’s some provinces over a ten-year time span (2007–201...

Impact of IFB uncertainty on dual-frequency code carrier divergence monitoring
KANG Kai, WANG Zhipeng, FANG Kun, ZHU Yanbo
2023, 49(9): 2463-2472. doi: 10.13700/j.bh.1001-5965.2021.0649
Abstract:

Code carrier divergence (CCD) monitor is one of the integrity monitors introduced by ground-based augmentation systems (GBAS), which is used to monitor the inconsistency between code pseudorange and carrier phase observations. Dual-frequency smoothing technology changes the test statistics and other...

Design and optimization of modular parabolic deployable mechanism
HE Tianyu, DONG Yang, WANG Hui, ZHAO Junpeng, WANG Chunjie
2023, 49(9): 2473-2481. doi: 10.13700/j.bh.1001-5965.2021.0652
Abstract:

As an important functional component of a satellite, a parabolic antenna is a basis for realizing remote sensing measurement and wireless communication. In order to solve the difficulty of configuration design and stiffness matching of modular parabolic antenna deployable mechanism, a configuration ...

Theory and performance research of DES and DDES in turbulent separation
SONG Hanqi, ZHANG Kailing, MA Ming, YAN Chao
2023, 49(9): 2482-2492. doi: 10.13700/j.bh.1001-5965.2021.0653
Abstract:

With the increasing complexity of flow structure in engineering, detached eddy simulation (DES) has become one of the most effective methods for turbulence simulation. DES is a hybrid method, combining Reynolds averaged Navier-Stokes (RANS) and large eddy simulation (LES) and thus possessing the hig...

An iterative pedestrian detection method sensitive to historical information features
DAI Peizhe, LIU Xiang, ZHANG Xing, SHANG Yanfeng, ZHAO Jingwen, WANG Shiyu
2023, 49(9): 2493-2500. doi: 10.13700/j.bh.1001-5965.2021.0665
Abstract:

Object detection algorithms based on deep learning usually need to use post-processing methods such as non-maximum suppression to filter the prediction box, and can not balance the detection accuracy and recall rate of the model in the crowded pedestrian scene. Although the iterative detection meth...

Attitude control law based on L1-ITD for a tail-sitter UAV
WANG Shuyang, ZHANG Jing, YANG Lingyu
2023, 49(9): 2501-2509. doi: 10.13700/j.bh.1001-5965.2021.0681
Abstract:

Aiming at the problem that the tail-sitter UAV is sensitive to wind disturbance in the vertical take-off and landing (VTOL) stage, an attitude control law based on L1-ITD is proposed. Firstly, a 6-DOF nonlinear model of a tail-sitter UAV in VTOL stage is established, and an L1 adaptive attitude cont...

Analysis of CO2 distribution characteristics in cabin of civil aircraft
GAO Jingcheng, CHEN Weijian, HU Wanjun, FENG Shiyu, LIU Haozheng
2023, 49(9): 2510-2517. doi: 10.13700/j.bh.1001-5965.2021.0683
Abstract:

The interior of civil aircraft cockpit is relatively closed, the air circulation is not smooth, the personnel density is large, and there are organic heat sources such as personnel and electronic equipment. It is essential to have a firm grasp of the flight envelope’s CO2 concentration, temperature ...

Weak supervision based blind remote sensing image mosaic quality assessment
PAN Linpeng, XIE Fengying, ZHAO Weiwei, ZHOU Ying, LIU Chang, WANG Yan
2023, 49(9): 2518-2526. doi: 10.13700/j.bh.1001-5965.2021.0694
Abstract:

A remote sensing image mosaic is an important research content of remote sensing image interpretation. However, affected by the imaging time, angle, and object texture, mosaic images often suffer inconsistent colors and structure dislocation. Aiming at the above quality problems, a double-branch net...

Taxiing deviation-correction control of a new variable-friction equipped-skid aircraft
WANG Yucheng, YIN Yin, LIANG Taotao, WEI Xiaohui
2023, 49(9): 2527-2538. doi: 10.13700/j.bh.1001-5965.2021.0700
Abstract:

Flat hypersonic aircraft are better suited to skid landing gear than wheeled landing gear because of its light weight and compact design. However, the inherent characteristic of the wheel skid layout causes the problem of heading instability during mid-speed taxiing. Aiming at the problem, a variabl...

Study on tail-slap load characteristics of high-speed projectile based on CFD/CSD coupling
XU Yuntao, TAN Dalin, YANG Chao
2023, 49(9): 2539-2546. doi: 10.13700/j.bh.1001-5965.2022.0939
Abstract:

A calculating approach based on the two-way analysis of computational fluid dynamics (CFD)/computational structure dynamics (CSD) coupling is devised to increase the predictability of the projectile’s tail-slap load. The main governing equation of fluid calculation adopts the Navier-Stokes equation ...