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    10 December 2024, Volume 45 Issue S2
    Model and Technology Development of Cross-domain CooperativeMission Planning for Ocean Autonomous Unmanned System
    WANG Liang, XU Tongle, XIAO Yujie, LI Ye, JIN Zirong, ZHENG Shengwu
    2024, 45(S2):  1-8.  doi:10.12382/bgxb.2024.0833
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    Cross-domain collaborative mission planning is the key technology and important support for the clustering, autonomization and multifunctionalization of unmanned systems. Focusing on ocean autonomous unmanned system, the basic concept, principle and characteristics of unmanned system cooperative mission planning are expounded, and the typical application cases of unmanned system cooperative mission planning are analyzed. The basic process and control structure of unmanned system cooperative mission planning are presented. A distributed mission planning model is constructed. The future research prospects are summarized by analyzing the existing problems in order to provide some reference for the construction and development of ocean autonomous unmanned system.

    Research Status and Prospect of Multi-domain Cluster Distributed Intelligent Cooperative Autonomous Control Technology
    GAO Zhifa, ZHOU Yu, YANG Hang, LAN Qing, LI Yuzhe, GAO Hui, ZHANG Zhenhua
    2024, 45(S2):  9-16.  doi:10.12382/bgxb.2024.0866
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    With the wide application of intelligent collaborative algorithm and autonomous technology in the field of air,space and sea equipment,the multi-domain cluster distributed collaborative autonomous control technology has also been deeply studied,and significantly improved the degree of intelligent autonomy of unmanned equipment.Based on the development needs of distributed intelligent autonomous control technology of multi-domain cluster,this paper reviews the relevant references related to multi-domain cluster distributed intelligent autonomous control technology and the research status at home and abroad.The relevant strategies,key research directions and advanced methods of multi-domain cluster collaborative autonomous control technology are deeply analyzed.The relevant key technologies and methods are summarized,and the future development trend is discussed.This paper provides a reference for improving the collaborative autonomous control ability of unmanned cluster system.

    Research on Firepower Compatibility Judgment for Cooperative Operation of High-energy Laser Weapons and Vertical Launching Ship-to-air Missile
    LIU Shenlin, ZHANG Chao, CHEN Zhihua
    2024, 45(S2):  17-24.  doi:10.12382/bgxb.2024.0870
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    Integrating the high-energy laser weapons into the arsenal of surface vessels is an inevitable trend.The firepower compatibility among high-energy laser weapons and vertical launching ship-to-air missiles is studied to maximize their effectiveness.For the firepower conflict between high-energy laser weapon and vertical launching ship-to-air missile the ballistic and damage models for laser weapons,the ballistic and dispersion models for ship-to-air missile,and the airspace resource models for laser weapon and ship-to-air missile are established.By analyzing the conflict scenarios between laser weapon and ship-to-air missile and considering the actual energy from the laser beams received by missile,the firepower compatibility discrimination is refined into incompatibility with conflict,compatibility with conflict,and compatibility without conflict.On the basis of this,a firepower compatibility discrimination is established for simulation.The simulated results indicate that the proposed model accurately describes the compatibility types between laser weapon and ship-to-air missile,providing effective information for resolving the conflicts.

    Research on a Judging Method for the Attack Intent of Drone Swarm
    SUN Haiwen, HAN Xiao, CHEN Ting, LI Dan, LI Ye, JIN Zirong
    2024, 45(S2):  25-35.  doi:10.12382/bgxb.2024.0851
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    The judgement of drone swarm attack intent involves many fuzzy and uncertain factors,and the judgement process belongs to the uncertainty reasoning process.A judging method based on discrete dynamic Bayesian network model is proposed for the judgement of drone swarm attack intent.According to the characteristics of drone swarm use,an indicator system for the determination of drone swarm attack intent is constructed.The continuous variables in the indicator system are transformed into the discrete variables by using fuzzy logic theory,and a model for drone swarm attack intent determination method is established.To address the problem of missing the indicator data in the evaluation process,a forward information repairing algorithm is used for information prediction and repairing.The simulated results show that the proposed method has a certain degree of fault tolerance,and can effectively judge the attack intent of drone swarm target based on the information before and after repairing,providing a reference for anti-drone swarm combat command decision-making.

    Overview on Operation Control and Planning Modeof Hubble Space Telescope
    ZHANG Aicheng, ZOU Xuemei, CHEN Xiang, ZHU Changming
    2024, 45(S2):  36-46.  doi:10.12382/bgxb.2024.0840
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    As the first large and complex on-orbit space astronomical observatory,the successful operation of Hubble Space Telescope(HST) is attributed to the leadership of NASA and the collaborative efforts of multiple control centers and agencies.This study delves into the multi-agency collaborative management mode of the Hubble mission,and analyzes the composition of flight operations personnel at the mission control center and their typical operational activities in detail.Additionally,the data uplink/downlink processing and transmission control mode of HST are examined,and the architecture of ground software system for HST and the upgrades and modifications since the mission’s inception are investigated.A comprehensive analysis is also conducted on the full planning process and periodic planning mode for Hubble’s astronomical observation missions.Based on the successful implementation experience of the Hubble mission,the specific and beneficial insights are proposed for China’s future space telescope mission.

    KAN-based Target Threat Assessment of Shipboard High-power Microwave Weapon
    XU Honghao, CAO Wei, ZHANG Yechao, CHEN Zhihua
    2024, 45(S2):  47-54.  doi:10.12382/bgxb.2024.0859
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    With the widespread application of modern electronic equipment,such as drones,on the battlefield,the high-power microwave (HPM)weapons have shown great potential in future maritime air defense operations.A key issue that needs to be addressed is the threat assessment when HPM weapons are used in conjunction with conventional shipborne air defense weapons.To tackle this,a threat assessment model based on the Kolmogorov-Arnold network (KAN)is established for evaluating the threat level of incoming targets by quantifying six core factors.Simulation experiments show that the KAN model maintains a threat assessment error below 0.036 with an average error of 0.0142,outperforming traditional BP network models and FABP network models.After incorporating HPM weapons,the corresponding quantitative indicators are adjusted,and the KAN model is used to predict the target threat values.The average target threat value is decreased by 0.0714.The HPM weapons can be usedsignificantly to enhance the air defense capabilities of naval vessels.

    Analysis of the Turbulent Properties of Flow in Water-jet Pump Based on Wall-modeled Large-eddy Simulations
    XU Hui, CHEN Zuogang, CAI Youlin
    2024, 45(S2):  55-64.  doi:10.12382/bgxb.2024.0850
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    Scale-resolving simulations are potential for accurate predictions of unsteady flows.Wall-modeled large-eddy simulation (WMLES)has the advantages of wide application and relatively low computational cost.However,the application of WMLES to the turbulent flow in water-jet pump is limited.The WMLES based on the analysis of turbulent length scales is applied to simulate the flow fields in a prototype pump and a modified pump,and the simulated results are compared to the experimental results.The head rise and torque coefficients predicted by the WMLES agreed well with the experimental data.The analysis of the turbulent properties of flows in the pumps demonstrate that the WMLES is capable of reproducing the horseshoe vortices,corner vortices,tip concentrating vortices and tip leakage vortices that are difficult for the conventional Reynolds-Averaged Navier-Stokes (RANS)method to reproduce.The horseshoe and corner vortices of the modified pump are much weaker than those of the prototype pump,and the limiting streamlines of the modified pump are smoother that those of the prototype pump.The lower dissipation of energy caused by the weaker vortices led to the higher efficiency of the modified pump.The results demonstrated that the WMLES based on the analysis of turbulent length scales could be effectively applied to predict the performance and turbulent properties of flow in the water-jet pump,which can provide the data support for the improvement of water-jet pump.

    The Influence Mechanism of Intake Structure on Scavenging Performance
    WANG Zengquan, LIANG Yongsen, WANG Wenxiao, LI Hong, SHI Dayu
    2024, 45(S2):  65-72.  doi:10.12382/bgxb.2024.0867
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    In order to explore the influence of various inset structures on scavenging performance,the orthogonal test of inset structure is carried out based on four inset structural parameters,namely,inlet wall thickness,inlet shape,inlet offset and number of inlets.The test results show that:the intake structure of a uniflow scavenging opposed-piston two-stroke diesel engine affects the overall performance of engine by influencing the swirl strength and flow resistance of intake air.The swirl intensity of the intake stream is adjusted by changing the inclination angle,the length and width of inclined plane of the intake structure.The total inlet contact surface affects the flow resistance by changing the intake angle of intake structure.The scavenging performance can be adjusted by changing the inlet flow intensity,and the exhaust gas backflow can be inhibited by changing the inlet flow resistance.It is found that the inlet wall thickness is a significant factor for regulating the scavenging performance of a opposed-piston two-stroke diesel engine.

    An Analytical Study of the Application of Additive Manufacturing Technology in US Navy Equipment Maintenance Support
    GU Jingyi, LI Yue, YANG Changsheng
    2024, 45(S2):  73-80.  doi:10.12382/bgxb.2024.0878
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    In order to study the application potential of additive manufacturing technology in naval equipment maintenance support,the US Navy’s use of this technology is analyzed in depth.The characteristics and process methods of additive manufacturing technology are briefly described.On this basis,the plan,status quo and technical challenges of using the additive manufacturing technology in US equipment maintenance support are elaborated.The testing and certification in the process of US Navy additive manufacturing and the new mode of maintenance support management system are mainly studied.The enlightenment and related recommendations for the development of future naval additive manufacturing technology used in equipment maintenance support are presented.

    Thinking About Prejudgment and Resolution of Cooperative Combat Fire Conflict of Foreign Directed Energy Weapons and Short-and Medium-range Air-defense Weapons
    LI Ye, TENG Zhe, WANG Liang, SUN Haiwen, GU Xiaodong, LU Fengbo
    2024, 45(S2):  81-89.  doi:10.12382/bgxb.2024.0892
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    The future air-defense operation situation is becoming more and more serious.The United States and Russia use the directed energy weapons and the short-and medium-range air-defense weapons to cooperate in combat,which makes the air operation of a single platform face an unprecedented risk of fire conflict.Focusing on the prediction and resolution of fire conflict in the cooperative combat of the directed energy weapons and the short-and medium-range air-defense weapons,the ballistic models of short-and medium-range air-defense weapons and directed energy weapons are constructed and the fire conflict criteria are analyzed by taking CHAMP HPMW,RAMvshort-range air-defense missile,Standard 2 medium-range air-defense missile and Phalanx close-in weapon system as examples,the ballistic models of medium-range and short-range air dense gun as example.The fire conflict resolution principles are designed,and the fire conflict resolution is verified based on the whole process of ballistic modeling and simulation in order to provide innovative ideas for the prediction and resolution of fire conflict among directed energy weapons and kinetic energy weapons.

    Research on the Demand Analysis and Development Status of Anti-fire Interference High Dynamic Infrared Imaging Technology
    LÜ Xiaoying, TANG Jiayu, WU Shilin, CAO Yuan, LIU Lin
    2024, 45(S2):  90-96.  doi:10.12382/bgxb.2024.0868
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    When using infrared imaging to detect the scenes of flames generated by high-temperature combustion of objects and high-temperature fragments generated by object explosions,the rapid increase in scene temperature within the infrared imaging field of view leads to an increase in the dynamic range of infrared imaging,the image saturation,the loss of detail information,and the submergence of weak targets by high-temperature backgrounds.Therefore,it is urgent to develop an anti-fire interference high dynamic infrared imaging detection technology.This article briefly introduces the current development status of high dynamic infrared imaging technology with anti-fire interference capability.On this basis,the development trend of high dynamic infrared imaging detection technology with anti-fire interference capability is analyzed.

    Progress on Environmental Perception Technology of Foreign Unmanned Surface Vehicles
    LI Dan, YU Shaozhen, YANG Huadong
    2024, 45(S2):  97-104.  doi:10.12382/bgxb.2024.0860
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    Unmanned surface vehicles (USVs) have high mobility,strong concealment,and extensive operational range,making them highly suitable for performing a wide array of tasks such as reconnaissance,anti-submarine warfare,search and rescue.Environmental perception technology,crucial for the operation of USVs,has attracted considerable attention.This paper conducts a survey on the development status of environmental perception technology for USVs at abroad,and define and analyzed the challenges in USV environmental perception through specific case studies.The current state of research on USV environmental perception technology is analyzed from the perspectives of both unimodal and multimodal perception,considering the sensory equipment utilized by USVs.Finally,the unresolved challenges in USV environmental perception technology are summarized,and its future development is prospected.

    An Optimized Threat Assessment Method for Aerial Target Groups
    TENG Zhe, LI Ye, QIU Qianjun
    2024, 45(S2):  105-112.  doi:10.12382/bgxb.2024.0891
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    The threat assessment method based on multi-contribute decision-making for aerial target groups is optimized to reflect the characteristics of target groups and improve the confidence of threat assessment.The threat assessment method and model for aerial target groups are established for the requirement of information compression of target groups.Then a dynamic intuition blur multi-contribute decision-making threat assessment method proposed in the paper is used to evaluate the combat abilities and threat level of aerial target groups.The dynamic intuition blur multi-contribute decision-making method is successfully used for threat assessment.Simulated results indicate that the dynamic intuition blur multi-contribute decision-making method enlarge the time dimension of multi-contribute decision-making method.It not only applies to the multi-contribute decision-making of single period of time,but also the multi-contribute decision-making of multi periods of time.

    Consensus Model and Collaborative Control Method of Large-scale Unmanned Cluster
    LI Shiying, DING Yinghe, SUN Haiwen, XU Zheng, LI Ye, TANG Enbo
    2024, 45(S2):  113-122.  doi:10.12382/bgxb.2024.0869
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    The unmanned systems are difficult to perform a mission in complex scenarios.The consensus models and collaborative control methods for large-scale unmanned cluster are studied by taking the emergence of swarm intelligence as the starting point of the research and the quadrotor drones as the research object.A neighbor selection mechanism and an adaptive attraction and mutual repulsion mechanism for the spatial partitioning of perception perspective are designed to generate the cluster spatial configuration.Combining the formation mechanism of social consensus in opinion dynamics,a view synthesis mechanism is constructed to achieve cluster speed synchronization.The autonomous group separation and aggregation rules are proposed and an obstacle avoidance method that combines active avoidance and safe strategy are proposed,so that the cluster size is flexibly adjusted to adapt to the dense obstacle environments.Simulated results show that the proposed method can be applied to a distributed cluster of 50 UAVs.In indoor,forest and urban environments with multiple obstacles,a cluster of 10 drones can safely cross an obstacle zone at a flight speed of 5m/s.The proposed method can be also applied to a distributed cluster of 4 UAVs which can safely traverse indoor obstacle zones,verifying the effectiveness of the cluster model.

    Investigation of Navigation Performance and Jet Flow Characteristics of Water-jet Propulsion Vessel in Shallow Water
    YANG Xi, FENG Yukun, CHEN Zuogang, ZHANG Yan
    2024, 45(S2):  123-132.  doi:10.12382/bgxb.2024.0847
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    The effect of shallow water on the navigation performance and jet flow characteristics of water-jet propulsion vessel is investigated,The navigation state of water-jet propulsion vessel and the patterns and mechanisms of jet flow under the conditions of different water depths are analyzed through numerical simulation.A numerical simulation method for the self-propulsion characteristics of water-jet propelled vessel is established using the Reynolds-averaged Navier-Stokes(RANS)equations to study the effect of water depth on the flow field around the vessel,jet flow morphology,and turbulence energy distribution.A regression prediction model for predicting the vessel behavior and jet flow characteristics is developed based on numerical calculations of vessel behavior and nozzle flow rates in different water depths.Results indicate that the shallow water blocking effects intensify as water depth decreases,increasing the differential pressure beneath the vessel and the stern inclination angle,while also increasing the recirculation velocity and draft around the hull.Additionally,the bow wave system grows and interacts with the stern wave system,leading to increased energy dissipation.The intersection point of jet flow and stern waves shifts forward with the decrease jn water depth,thus increasing the radial diffusion and vorticity,and decreasing the propulsive power,while increasing turbulence energy and water disturbance.These findings provide a scientific basis for the practical application of water-jet propulsion technology in shallow water conditions to improve the efficiency and safety of water-jet propelsion vessels in complex aquatic environments.

    Development of Space International Cooperation:New Trends,New Characteristics,and Relevant Considerations
    JI Fance, LI Shuai, QIAN Kun
    2024, 45(S2):  133-138.  doi:10.12382/bgxb.2024.0879
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    The accelerated evolution of the unprecedented changes unseen in the past century has profoundly affected the development of international cooperation in space in the world and put forward new requirements for China’s future international cooperation in space,which urgently needs to be further improved.In order to provide reference for China’s international space cooperation activities,the new trends and characteristics of the development of international space cooperation in the world are studied and overviewed.The new trends in the development of international cooperation in world spaceflight are analyzed mainly from the perspectives of strategic traction,legal promotion,international rules and commercial spaceflight.The new features of the development of international cooperation in world spaceflight are summarized from different dimensions,such as cooperation environment,cooperation relations and cooperation subjects.In the light of the new trends and characteristics of the development of international cooperation in spaceflight in the world,the paper puts forward the community of human destiny as the core concept of China’s international cooperation in spaceflight,as well as the corresponding concrete practical measures.

    Comprehensive Calibration and Data Application of High-orbit Ocean-color Satellite
    CHEN Zhuoyi, SUN Rongyang, WANG Fuhai, LI Zhupeng, YUE Ronggang, WANG Chenglun
    2024, 45(S2):  139-145.  doi:10.12382/bgxb.2024.0673
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    High-orbit ocean observation satellites are effective tools for monitoring the short-term changes in marine environments and the sudden disasters near coastlines.This paper focuses on the comprehensive calibration and data application of high-orbit ocean color satellite technology.The current status and development trends of ocean color sensors in orbit are discussed,and the technical challenges,such as atmospheric correction,radiometric calibration,and sensor stability,are presented.To address these challenges,a unified calibration approach integrating ground-based,laboratory-based and on-orbit calibration methods is proposed.This approach ensures the high-precision calibration of sensors under different phases and conditions.The ground-based calibration,utilizing the standard radiometric sources and precise measurement equipment,ensures the initial accuracy of on-orbit sensors.Meanwhile,the on-orbit calibration involves the continuous monitoring and correction to maintain the long-term stability and data consistency of the sensors.The future developing directions of high-orbit ocean color satellite technology are summarized,and the importances of multisource remote sensing data integration,intelligent calibration algorithms and autonomous on-orbit correction techniques are emphasized.The research aims to provide more accurate and reliable data support for ocean observation,promoting the rwidespread application of high-orbit ocean color satellite technology in environmental monitoring,resource management,and scientific research.

    Design of Inter-satellite Separation of China’s First All-electric Communication Satellite
    PAN Yuqian, FANG Yaopeng, WEI Qiang, WANG Min, SUN Guopeng, LIU Cuicui, LIANG Xingang
    2024, 45(S2):  146-152.  doi:10.12382/bgxb.2024.0880
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    AP-6E satellite is the first domestic all-electric communication satellite,which is also the first communication satellite in the world to realize the autonomous orbit transfer from low earth orbit to geosynchronous orbit.The separable propulsion segment is utilized to realize the rapid orbit transfer via the chemical propulsion system,then the segment is separated and de-orbited,finally the remaining tasks of the satellite are preformed solely by the electric propulsion system.Therefore,the inter-satellite separation is the key to the success of this mission.The design of the connection and separation mechanism of AP-6E is introduced,and the stress margin of connection and the near-field and far-field safeties of separation process analyzed in order to systematically expound the experience of the engineering practice of the all-electric propulsion platform carried by the low-cost launch vehicle,which is of certain significance for the subsequent projects.

    System Safety Analysis of Unmanned Ground Vehicles Based on STPA Method and Bow-Tie Model
    XIAO Yang, SU Bo, JI Chao, YANG Dezhen, ZHOU Tong
    2024, 45(S2):  153-161.  doi:10.12382/bgxb.2024.0871
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    As the potential applications and strategic value of unmanned ground vehicles(UGVs)in complex operational environments become increasingly prominent,the safety of their autonomous actions is of paramount importance.This paper proposes a system safety analysis method for UGV,which combines the system-theoretic process analysis(STPA)method and the Bow-Tie model.Focusing on the safety of teleoperated UGVs,the STPA method is utilized to identify the unsafe control actions(UCAs)within the UGV system and their associated latent risks.Subsequently,the Bow-Tie model is utilized to analyze the event chain from loss causation scenarios to potential accident consequences,thereby delineating the risk propagation and diffusion pathways.Ultimately,the active and passive safety stratified control measures are determined based on the Bow-Tie analysis,and the system safety management is realized through an autonomous safety controller.

    Modeling and Prediction of Driver’s Steering Control Behavior for Stepless Steering Tracked Vehicle
    DU Yunsheng, WANG Wenshuo, WEI Yuan, CHEN Huiyan
    2024, 45(S2):  162-169.  doi:10.12382/bgxb.2024.0877
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    Reforming the current manned tracked vehicles into the unmanned tracked vehicles is one effective way to develop the unmanned tracked vehicle.To this end,a data acquisition system is designed to collect the vehicle state and driver’s operation data.Based on the collected data,the driver’s steering behaviors during the tracked vehicle’s operation are clustered and analyzed based on the Gaussian mixture model(GMM),and a steering control behavior model is established.Based on different steering categories from GMM,a prediction model for the driver’s steering operation is trained by taking the running speed and steering angle deviation of vehicle as model inputs and the turning angle of hydraulic motor swinging arm as the predictive truth value of steering control.The proposed predsiction model is used for the statistical modeling and prediction of driver steering behavior in the in real cross-country environment.Experimental results show that the proposed steering control model can predict the driver’s steering behavior accurately.

    Airocraft Research on Thermal Vibration Test of Typical Rudder Structure
    WANG Pengfei, LIU Zhen, ZHOU Changwei, DANG Tianjiao
    2024, 45(S2):  170-175.  doi:10.12382/bgxb.2024.0865
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    In response to the complex and variable dynamic response of aircraft control surfaces in hot environments,a typical control surface structure is studied. A heating vibration test platform for a typical control surface structure is designed and built for thermal vibration tests on the control surface under different thermal environments in order to obtain the transfer function of the structure under different thermal environments.The research results indicate that the test bench can provide relatively uniform heating on both sides of typical rudder structure,and restore the response characteristics of the structure during real flight by applying external loads through a vibration table.The experimental results indicate that the test method can be used for the combined thermal-vibration tests on aircraft at temperatures ranging from 20℃ to 600℃.The test method provides important engineering significance for the study of aircraft thermal-vibrationtests.

    Experimental Research on the Impact of Flying Object on Prestressed Reinforced Concrete Target Plates
    DONG Jun, JIANG Di, SUN Liang, SONG Mengyan, CHEN Fei, LIU Mengsha, REN Yike
    2024, 45(S2):  176-185.  doi:10.12382/bgxb.2024.0858
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    Based on the application research background of large aircraft impact,the experimental research is conducted on the impact of flying object on a prestressed reinforced concrete target plate.The scaled samples equivalent to flying object and prestressed reinforced concrete target plates are designed using a geometric scaling ratio of 1:6.Finite element analysis software is used to construct the collision models and calculate the impact damage effects of two scaled samples with different structures on the target plate at different speeds.A physical loading test is conducted using an air cannon,and the critical penetration velocity of two scaled samples on 200mm thick prestressed reinforced concrete is obtained by comparing the test results with simulated results.This provides basic data for intuitive prediction/evaluation of the impact response and failure mode of prestressed reinforced concrete containment in nuclear power plants,and also provides design references and basis for prototype collision test schemes.

    Study on the Assessment of Damage level of Explosion Damage Elements against Personnel
    LI Yin, DENG Guoqiang
    2024, 45(S2):  186-192.  doi:10.12382/bgxb.2024.0857
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    Personnel are a critical factor in warfare.The damage effects of three types of damage elements,namely,shock wave,thermal effect and fragments,against personnel,are assessed based on the anti-personnel criterion through numerical simulation,experiment and theoretical computation tools.A damage zone of shockwave overpressure against personnel is delineated,and the relationship between scaled blast distance and personnel damage level is established,resulting in the minimum scaled blast distance of damage to personnel being 8.155m/kg1/3.The spatial distribution of explosion thermal effect is calculated,and the free-field non-fuel air explosive or thermobaric bombs are not suitable for separate assessment of thermal effect on the personnel killing effect is put forward.The generation process of fragments is numerically simulated to obtain the quality,quantity and velocity of fragments.The simulated results are compared with the theoretically calculated results to assess the damage effect of the specific kinetic energy of fragments to personnel.The conclusions can provide reference for the design of warhead and the protection of battlefield personnel.

    Numerical Simulation and Experimental Study on Damage Effect of Prestressed T-shaped Beam under Blast Load
    ZHANG Jiansheng, JING Jianbin, SUN Hao, WANG Xiquan, LI Bo
    2024, 45(S2):  193-198.  doi:10.12382/bgxb.2024.0961
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    The damage effect of prestressed T-shaped beam under blast load is studied.A 1:3 complex steel-concrete structure finite element model of prestressed T-shaped beam is established by using nonlinear finite element software.The mesh size matching and coordination between reinforced beam elements and solid concrete elements are designed,along with the coupling among the prestressed steel strand,beam rib reinforcement,edge plate reinforcement and cross-beam reinforcement.Then cooling prestressed contraction method are used to flexibly control the accurate loading of value transfer between prestressed and T-shaped beam elements.The finite element simulation results are compered with the experimental results.The comparison result indicates that the numericial simulation and experimental damage situations are basically consistent,and at the same position,the relative error between the simulated value of shock wave overpressure and the test value is less than 20%,which verifies the effectiveness of the numerical simulation model.It can provide the simulation methods and data support for the vulnerability analysis and explosion resistance design of subsequent steel-concrete frame structures.

    On the Construction of a Trans-media Water-entry Test System for Projectile
    HAN Xiangdong, WANG Xiquan, LI Chao, CHEN Junbiao, LI Junzhi, FENG Huiyong, WEI Xuemei
    2024, 45(S2):  199-207.  doi:10.12382/bgxb.2024.0950
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    To comprehensively carry out the trans-media water entry test of projectile under the mutual coupling of different motion peculiarities and various operating environment properties,a multifunctional trans-media water-entry test system is built.The test system includes a launch subsystem,a parameter measurement subsystem,and a medium property subsystem.The launch subsystem is mainly used for the trans-media water entry test of projectile under the mutual coupling of multiple factors,and is checked via numerical simulation.The results indicate that the launch subsystem is safe and reliablem,and could be used to perform tests normally.The parameter measurement subsystem is used to qualitatively observe the temporal and spatial evolution of cavitation bubbles during the trans-media water entry process of projectile via a high-speed camera and quantitatively measure the real-time change of acceleration by a acceleration sensor.The medium property subsystem is used to build an operating environment with different viscosities and densities.Overall variations of bubbles and accelerations obtained from tests indicate that the test system could be fully employed to perform trans-media water entry test for the projectile.

    The Virtual Test of Impact Damage on Weapon SystemBased on SPH Numerical Simulation Method
    LI Pengfei, XIA Hongli, HOU Chuanyu, ZHOU Yuqi, MIAO Haibin
    2024, 45(S2):  208-214.  doi:10.12382/bgxb.2024.0959
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    The problem of impact damage widely exists in various types of weapons and equipment,and seriously affects their use and lifespan.Currently,there is no universally applicable basic model for virtual experimental research on impact damage.This article focuses on the construction of basic model for impact damage virtual testing,and discusses the basic principles of smooth fluid dynamics and the application of its numerical simulation method in impact damage virtual testing.An improved smoothed particle hydrodynamics(SPH)numerical calculation model is constructed,and the particle processing and material boundary treatment of physical models are discussed in detail.Simulation calculations are conducted on the impact of typical rigid particles on the impact copper target plates,verifying the reliability and accuracy of the simulation.The damage situations of target plates impacted by the rigid particles with different edges and angles are compared and analyzed,fully demonstrating the applicability of the SPH method in virtual impact damage testing.

    Damage Characteristics of Typical Ship Targets Subjected to Underwater Explosion
    YAN Xiaojun, SUN Hao, MA Lin, ZHANG Xuhui, WU Xi, YONG Shunning
    2024, 45(S2):  215-221.  doi:10.12382/bgxb.2024.0960
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    As the main platforms in maritime warfare,the warfare ships face various threats,among which underwater explosion is the most destructive one.In order to study the structural damage and dynamic response characteristics of ship under underwater explosion,a simplified model of Arleigh Bruke-class destroyer is established,and the underwater explosion is numerically simulated using nonlinear finite element software.The process of ship damage at different explosion distances and the overload acceleration at key locations are analyzed.The results show that the large local damage fracture of ship is the main damage form of near-field underwater explosion,and the whole whiplash movement of ship is the main damage form of far-field underwater explosion.

    Skid-steering Wheeled Vehicle Model Coupled with HydraulicDrive system and Its Dynamic Characteristics
    LIU Qihui, WU Wei, PAN Feng
    2024, 45(S2):  222-230.  doi:10.12382/bgxb.2024.0061
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    Skid-steering wheeled vehicle has a wide range of applications. Understanding the impact of drive system on the vehicle driving and steering performance is the basis for forward design. In response to the design and analysis requirements of hydraulically-driven skid-steering wheeled vehicle, a coupling simulation model of hydraulic drive system and vehicle dynamics system is established based on the principle of the hydraulically-driven skid-steering wheeled vehicle systems. Combined with the specific vehicle parameters, the characteristics of the vehicle driving and steering conditions are simulated and analyzed to obtain the dynamic response characteristics of hydraulic driving system during vehicle driving. The simulated results of the model are verified through the actual vehicle. The results show that time-varying parameters such as road resistance, vehicle speed and driver operation have a great impact on the pressure of hydraulic driving system, which is strongly related to the dynamic steering resistance. The coupled simulation model can be used for the coupled simulation of vehicle motion state and hydraulic driving system state and the coupled analysis of hydraulic driving system characteristics and vehicle dynamics characteristics.

    Key Technology of Safe Disposal of Unexploded Ordnance
    YUN Kang, DANG Feng, HAN Xiangdong, LI Yunchao, LIU Yuzhao, LI Lu, CHENG Cheng
    2024, 45(S2):  231-239.  doi:10.12382/bgxb.2024.0683
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    Unexploded ordnance refers to ammunition that has been disarmed, detonated, ignited or otherwise prepared for use or has been used, and has not exploded due to fuze failure, functional failure, design defects or other reasons after igniting, throwing, launching or burying for various reasons. The research status of safety disposal technology of unexploded ordnance at home and abroad is described,the unexploded ordnance detection technologies, such as magnetic detection, sound-magnetic compound detection and optical detection, and the non-contact disposal and destruction technology principles, such as burning treatment, blasting destruction, cutting treatment, are analyzed, and the advantages and disadvantages of different detection and disposal technologies and their application scenarios are summarized. At last, it is pointed out that the detection and disposal technologies of underwater unexploded ordnance are the focus of the current national defense field, and also the research hotspot. The research on key technologies of safe disposal of unexploded ordnance can provide theoretical basis for unmanned, safe and environmentally friendly detection and disposal of unexploded ordnance in the future.

    Inertial-based Deep-coupling Navigation Method with Embedded Flight Dynamics
    YANG Ziao, QU Qifu, SUN Haiwen, LI Ye, JI Zhentao
    2024, 45(S2):  240-250.  doi:10.12382/bgxb.2024.0780
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    To study the autonomous navigation method of high dynamic flight vehicle that does not rely on satellites,a flight dynamics model of high dynamic flight vehicle is established.The numerical integration method is used to solve the trajectory information of high dynamic flight vehicle,the flight error characteristics of high dynamic flight vehicle is analyzed,and generate the virtual inertial navigation data is generated.A navigation solution method using the dynamic weighting of measured inertial navigation data and virtual inertial navigation data is proposed based on the characteristics of flight errors,and the “velocity+attitude” matching Kalman filter method is used to further suppress the navigation errors.The inertial-based deep-coupling navigation method with embedded flight dynamics is proposed and proven through simulation.The results show that the proposed deep-coupling navigation method can significantly improve navigation accuracy.The improvement in navigation performance of the proposed method reaches 97.1%,72.9%,and 40% under different degrees of preset flight trajectory deviation.

    Test Research on Damage Effect of Full-size Shaped Charge Warhead with Conical-spherical Combined Liner
    ZHOU Fangyi, ZHAN Famin, HUANG Xuefeng, JU Xiangyu, JIANG Tao
    2024, 45(S2):  251-258.  doi:10.12382/bgxb.2024.0084
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    In order to improve the damage ability of shaped charge warhead, a kind of full-size shaped charge warhead with conical-spherical combined liner and a double-layer target plate with water interlayer are designed based on the initiation mechanism of shaped charge warhead with conical-spherical combined liner. The underwater explosion damage test of warhead to target plate is done. The test result shows that the shaped charge warhead can penetrate through the double-layer target plate with water interlayer (10mm non-pressured shell+1000mm water interlayer+40 pressured shell), and the penetration depth of it to target plate is more than 130mm. Therefore, the combined liner structure is propitious to improve the damage effect of warhead on double-layer target plate with water interlayer,which provides an effective way to improve the power of warhead.

    Aerodynamic Characteristics and Control Mechanisms of Spoilers for Multi-body Tail-controlled Projectile
    LUO Xinrui, ZHANG Meng, DENG Zhihong, SHEN Kai, JIANG Zhihao
    2024, 45(S2):  259-270.  doi:10.12382/bgxb.2024.0781
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    In modern warfare, the demand for long-range precision strikes has increased, and the traditional unguided weapons are no longer sufficient to meet these needs. Guided weapons are receiving increasing attention. The aerodynamic characteristics of spoilers, as control actuators, under different conditions have been insufficiently understood, and their control mechanisms are not yet well-defined. The aerodynamic performance variations of spoilers at different heights, spans and axial positions, as well as their principles are investigated through numerical simulation and trajectory analysis. The causes of variations in additional forces and moments at different Mach numbers are analyzed through the use of shadowgraphs,streamlines,and other diagnostic methods.The study results indicate that the different parameters of spoiler have significant impacts on the additional forces,moments and control drag ratio. Specifically, the additional axial force directly affects the range of projectile, while the additional normal forces and moments have influences on the correction capability of projectile. This research provides important reference for the future design and optimization of spoiler and control system.

    Analysis of Complete Period Free Rotational Vibration Motion of a Tail-controlled Dual-spin Projectile
    ZHONG Ding, JI Zhentao, YANG Pengxiang, ZHANG Xinye, JIANG Zhihao
    2024, 45(S2):  271-282.  doi:10.12382/bgxb.2024.0782
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    Recently, the guided transformation-based dual-spin configuration has become an effective means to improve the accuracy of ammunition strikes.To study the complete period free disturbance motion of a new type of tail-controlled dual-spin projectile, a 7 degrees of freedom ballistic model is established based on the ideal bearing assumption and non-roll coordinate system.The ballistic equations are linearized using the coefficient freezing method and small disturbance assumption.The complete period free disturbance motion equations are derived and represented in a state space form.A feature point on the ideal trajectory is selected.The motion modal for the complete period free disturbance near the feature point is obtained by numerical calculation method.The forms of free disturbance motion under different initial deviation values are discussed.The results indicate that the dual-spin projectile exhibits strong coupling characteristics in longitudinal and lateral motions.Similar to conventional projectiles, the free disturbance motion of dual-spin projectiles can still be divided into two stages: long period and short period.But the difference lies in the slow convergence of the angle of attack offset, and the modal amplitudes of different angle of attack offsets have different distribution patterns.The research results lay the foundation for further studying the angular motion and designing the guidance law.

    Static Power Field Reconstruction Method for Natural Fragmentation Warhead
    FENG Changlin, SHI Rui, ZHANG Bing, WANG Xiaodong, LIAO Shasha
    2024, 45(S2):  283-292.  doi:10.12382/bgxb.2024.0838
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    The warhead power is the load input for the calculation of damage effect. The accurate construction of a static power field model for warhead becomes an important task to evaluate the accuracy of damage assessment task. Based on the unique characteristics of natural fragmentation warhead, a method for reconstructing the static power field model for warhead is proposed by numerical simulation, theoretical analysis and experimental verification. That is, an initial model of fragmentation power field is constructed based on the calculated results of the numerical simulation model, an initial model of the shock wave power field is constructed based on the classical analytical theory, and the key characteristic quantities of the power field are corrected item by item based on the sample data of the experiment. Through the case calculation, it is shown that the power field model of natural fragmentation warhead established by using the proposed reconstruction method can accurately describe the actual warhead power characteristics, and can be effectively applied in the related fields of warhead performance evaluation and weapon equipment effectiveness evaluation.

    Current Status and Issues of the Safety Protection System for the Production Systems Engineering of Burning Explosives
    MA Zhiwei, LI Yuan, GUO Mingzhe, SUN Mou
    2024, 45(S2):  293-304.  doi:10.12382/bgxb.2024.0931
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    The air shock waves, fragments, thermal radiation, explosion effects and propagation patterns of explosive system, as well as the allowable levels that personnel, equipment and other burning explosives in the explosive system can withstand are analyzed, and the typical engineering protective measures for explosive manufacturing are discussed. These measures include sealed anti-explosion structures, personnel shelters, protective barriers, and safety distances. Based on engineering practice experience, with the aim of saving land resources and further balancing the effectiveness and economic rationality of engineering protection, it is proposed that the following issues need to be continuously studied and improved: the quantitative evaluation method for combustion and explosion effects in different scenarios, the quantitative evaluation method for the degree of destruction caused by accidents, and the risk-acceptable criteria and quantitative evaluation and optimization method for the effectiveness of engineering protection measures.

    Explosive Damage Law and Rapid Calculation Model for RC Bridge Piers
    JIANG Haojie, PENG Yong, SUN Yuyan, WANG Ziguo, XU Jiapei
    2024, 45(S2):  305-316.  doi:10.12382/bgxb.2024.0966
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    For the prediction of damage effect of reinforced concrete (RC)bridge piers subjected to explosion,the effects of explosive equivalent,explosion distance,explosion height,pier diameter,longitudinal reinforcement rate,hoop reinforcement rate,axial compression ratio and other parameters on the damage pattern and residual bearing capacity of RC bridge piers are discussed in detail through numerical simulation,and the damage law and residual bearing performance of a typical land-based RC bridge pier under the action of explosion load are obtained.As the explosion height increases,the ground reflection effect is weakened so that the residual bearing capacity increases,and an appropriate increase in the axial compression ratio can enhance the residual bearing capacity of bridge pier.By using the sub-coefficient method and taking the residual bearing capacity of RC bridge piers after explosion as an indicator,a formula considering a wide range of explosion parameters,the bridge pier component parameters and the initial stress state is proposed for calculating the damage effect of round RC bridge piers,which can quickly predict the damage of typical bridge piers subjected to explosion.

    A Reconnaissance Task Allocation Algorithm for Air-Ground Heterogeneous Unmanned System
    SUN Yujie, SU Bo, DUAN Leyi, JI Chao, YANG Chaonan
    2024, 45(S2):  317-328.  doi:10.12382/bgxb.2024.0319
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    Aiming at the reconnaissance task allocation of air-ground heterogeneous unmanned system,this paper proposes a two-stage mixed task assignment(TMTA)algorithm for reconnaissance tasks and communication relay tasks.An alternative set of reconnaissance position and communication relay position are constructed based on the reconnaissance distance,communication relay distance and target position.An reconnaissance and communication relay tasks dispatching model is built by taking the task timeliness and path cost as the objective functions,in which the combining reconnaissance/communication relay task completion constraints,coupling constraints between task location selection/task execution time and task paths,and path continuity constraints,etc.,are considered.To solve the nonlinearity of the model,the advantages of set coverage algorithm,Hungarian algorithm,and genetic algorithm are synthesized to design a TMTA algorithm,which realizes the efficient solution of the model.The proposed method is validated through experiment.The experimental results show that the proposed algorithm outperforms the baseline dispatching algorithm in terms of task timeliness and path cost.