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Table of Content

    27 June 2023, Volume 41 Issue 3
    Civil Aviation
    Management strategy of the urban UAV based on digital airspace system
    CHEN Zhijie, ZHU Yongwen, LIU Yang
    2023, 41(3):  8-12. 
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    With the popularization of the unmanned aerial vehicle (UAV) industry, the traditional mode of air traffic manage ment (ATM) is not suitable for the air traffic operation in the urban environment. The continuous extension of in formation technology brings more possibilities for low altitude airspace management. From the aspects of policy system, UAV control and digital construction of low altitude, a management plan of urban UAV is constructed based on the digital airspace system of low altitude. Firstly, the core difficulties and key scientific issues faced in the current management of urban UAV are summarized from the perspective of UAV and ATM. Then, key tech nologies concerned about policy system, UAV control, digital construction of low altitude are researched. Finally, effective suggestions for the management of urban UAV are proposed to promote the development of new ad vanced air traffic modes in the future
    Rerouting in severe weather based on improved artificial potential field method
    XIE Chunsheng, ZHANG Xu
    2023, 41(3):  13-18. 
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    Aircraft are susceptible to the impact of severe weather during the flight, which will cause property damage and pose a threat to the safety of the life of personnel. For flight safety, the aircraft needs to be rerouted to avoid severe weather in the route. Therefore, this paper studies the problem of aircraft rerouting, combining with the constraints of various aircraft performance and flight safety, a rerouting planning model with the shortest rerouting path as the goal is established. A rerouting path planning algorithm based on improved artificial potential field method is proposed. Secondly, in order to prevent the problem of unreachable target point in traditional artificial potential field method, the repulsion function is improved, and the simulated annealing algorithm is merged to solve the local minimum problem. Finally, through the simulation of the algorithm, the rerouting path is reduced by 18.52% compared with the traditional method. This algorithm can provide a theoretical reference for the air traffic control department to divert aircraft under severe weather.
    A weak signal acquisition method for BeiDou GEO satellite
    LYU Zipeng, ZHANG Jianjun, LYU Lin, HAN Ming, DENG Qi
    2023, 41(3):  19-24. 
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    The D2 navigation data broadcast by the BeiDou geostationary earth orbit (GEO) satellite may change every 2 ms.In weak signal environment, the usual acquisition algorithm cannot effectively capture the signal. To solve this problem, a weak signal acquisition method based on navigation data estimation is proposed. The capture strategy of this method can be adjusted according to the signal quality, by quickly and accurately estimating the navigation data, thus the impact of navigation data jump on capture sensitivity is reduced. The simulation results show that, for the BeiDou GEO signal with length of 60 ms and signal-to-noise ratio of -34 dB, the acquisition success rate of this method is 80%, and the acquisition time is equivalent to that of the full-bit method.

    Vulnerability assessment of ATC operation system based on cloud model
    YUE Rentian, ZHANG Zhibo
    2023, 41(3):  25-30. 
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    In order to evaluate the vulnerability of air traffic control (ATC) operation system, this paper first analyzes 1 018 unsafe incidents of ATC in 2011-2018, classifies the causes, and extracts the influencing factors of vulnerability of ATC operation system. According to the four aspects of controller, equipment, environment and management of ATC system, as well as five parts including flight crew, airport support, aircraft, dispatch and military aviation activities in operation environment, a total of 28 vulnerability assessment indicators of ATC operation system are summarized. Then, the comprehensive weight is obtained by AHP and entropy weight method. Considering the vulnerability influencing factors, the features of system disturbance are evaluated by using the cloud model with fuzzy and random characteristics. After scoring by Delphi method, the forward cloud generator is applied to draw the cloud chart which can directly reflect the vulnerability level of each indicator. Finally, the evaluation results are compared with the fuzzy comprehensive evaluation method. The results show that the vulnerability level of ATC operation system of North China Air Traffic Management Bureau tends to be relatively high, with frequent occurrence of unsafe events, among which military aviation activities and controller factors have greatest effect.
    Influence of terrain on low-level windshear at the approach-departure paths of HKIA
    HUANG Yanni , CHEN Feng , Pak-wai Chan
    2023, 41(3):  31-40. 
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    To identify the prone airspace of complex terrain-induced low-level windshear at Hong Kong International Air port(HKIA), large eddy simulation(LES) method was used to simulate the wind field of the airport and its surrounding terrain. The wind speed changes at the take off and landing paths of three runways under the background of east, southeast, south and southwest wind were compared combined with wind speed cloud map, and the causal relationship between the terrain and the wind field distribution was analyzed. By comparing the results with the control test without terrain, the F-factor (headwind) and 7-knot standard (crosswind) were employed to identify the prone regions of low-level windshear at the airport runway. The results showed that the east wind was easy to cause the temporal and spatial variation of the headwind speed at the take off and landing paths of the aircraft.

    The southwest wind affected the headwind speed at the landing path on the east side of the runway, but had little effect on the take-off path on the west side of the runway. Under the background of southeast wind and the south wind, the crosswind in the low altitude section at the approach-departure paths of the three runways were signifi cantly affected by the terrain. According to prone airspace of the low-level windshear at take off and landing paths of three runways, the influence range of topographic factors on low-level windshear of HKIA was obtained, which can provide active avoidance measures and suggestions for airport windshear risk prevention and control.

    Research on the internal influencing factors of pilots′ unsafe behaviors
    WANG Yonggang, CHE Zhuojun
    2023, 41(3):  41-46. 
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    In order to study the internal influencing factors and mechanism of pilots′ unsafe behaviors, and reduce their unsafe behaviors, internal influencing factors are identified from three stages of the information cognition process of pilots (information perception-information decision-information utilization), also the impact of dedication on the information cognition process and unsafe behaviors of pilots are analyzed, based on information cognition theory and literature analysis. Secondly, the interrelationship between internal influencing factors and key factors that influenced pilots′ unsafe behaviors are determined by using Grey-Dematel method. The results show that the internal influencing factors of pilot′s unsafe behaviors include response time, attention, memory, flight technology, risk tolerance, risk attitude, fatigue and engagement, among which memory, flight skills, risk tolerance, fatigue and engagement are the cause factors, and respense time, attention and risk attitude are the result factors, fatigue, attention and flight skills are the key internal influencing factors of pilots′ unsafe behaviors.
    Selection of the most critical conditions for dynamic impact test of aviation seat
    WANG Yafeng, LIU Jijun
    2023, 41(3):  47-52. 
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    In order to determine the most critical condition for dynamic impact test of aviation seat, this paper carried out the analysis and calculation of dangerous condition selection for a certain type of aviation seat in two stages of displacement loading and impact loading, based on the study of Article 25.562 of Chinese civil aviation regulations(CCAR), Federal Aviation Administration(FAA) AC 25.562-1B, Society of Automotive Engineers (SAE) AS8049B and other relevant airworthiness regulations and technical standards. The most critical condition for dynamic impact under various predeformation of the floor during the airworthiness test is evaluated and the forensics test of airworthiness is completed according to the conclusion. This method can be applied to the selection of critical conditions before dynamic impact test of various types of aviation seats.
    Numerical simulation of the effect of water mist nozzle spray angle on fire suppression in semi-enclosed aircraft cabin
    GAO Jianshu , WANG Qingqiang
    2023, 41(3):  53-58. 
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    In this paper, the model of aircraft real fire training simulator is built by fire dynamics simulator(FDS) software, and the influence of water mist nozzle spray angle and flow rate of fire nozzle on fire fighting efficiency in semienclosed cabin are studied. The effectiveness of fire suppression, the process of heat and mass transfer are analyzed based on factors such as flame suppression time, gas concentration and temperature differences. The results show that the temperature attenuation rate can be increased by increasing the flow rate of fire fighting water or reducing the nozzle spray angle. In addition, as the nozzle spray angle increases, the O2 concentration in the cabin will decrease and the CO2 fraction will increase. By studying the changes in temperature and gas concentration inside the cabin caused by the nozzle spray angle and fire water flow rate, theoretical support can be provided for firefighters to conduct firefighting training
    Optimization of strength of safety box buckle based on response surface model
    SHI Yongsheng, DU Kun, LI Sha
    2023, 41(3):  59-64. 
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    Taking the safety box buckle as the research object, based on the response surface optimization theory, regression equations is firstly constructed to optimize the objectives, and Box-Behnken design (BBD) method is applied to design random experiments. The different lengths, widths, thicknesses, and fillets of the bottom side of the buckle are selected as parameters for model design, modeling and finite element simulation analysis are performed ac鄄 cording to the design parameters. The regression equation between the parameters and the response is construct鄄 ed, and the maximum stress is taken as the optimization goal to optimize the solution. Finally the optimized plan is verified, which can provide a novel optimization method for the design of the buckle.