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Table of Content

    28 December 2022, Volume 50 Issue 6
    SPECIAL COLUMN
    Overview of Hypersonic Weapon Development and Defense System Research in Near Space
    Hong-yu LI, Tong YIN, Xiao-biao DUN
    2022, 50(6):  1-10.  doi:10.3969/j.issn.1009-086x.2022.06.001
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    For the first time, Russia used the "Dagger" hypersonic weapon to destroy a large underground warehouse in Ukraine in combat, causing the world to pay more attention to hypersonic weapons and a growing sense of urgency. Hypersonic weapons have the advantages of fast flight speed, strong maneuver ability and difficult flight trajectory prediction, which makes the traditional missile defense system "paralyzed overnight". As countries around the world accelerate the weaponization of hypersonic technology, the hypersonic weapon defense system is also being built simultaneously. Aiming at the defense problem of foreign hypersonic weapons, the development status of foreign hypersonic weapons and the construction of hypersonic weapons defense system in the United States and Russia are analyzed in depth, and the development direction of foreign hypersonic weapons defense system construction is sorted out. The research results can promote the development of advanced defense technology.

    Threat Analysis Methods of Actively Approaching Spacecraft
    Li-jun WU, Hao ZHANG
    2022, 50(6):  11-18.  doi:10.3969/j.issn.1009-086x.2022.06.002
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    With regard to the non-cooperative actively approaching spacecraft with maneuverability, a threat index calculation model to analyze the threat of the chaser to the target is proposed. We extract the impulse and the time required for rendezvous based on two impulses Lambert algorithm as threat elements after analyzing the mission mode of the chaser. The most threatening route is selected to weigh the impulse and time in order to calculate the comprehensive threat index. Simulation results show that the threat index of the chaser is very sensitive to the changes of orbital elements. Comparing the commonly used relative distance index, the threat index can identify the maneuver intention more quickly according to its trend. Under the complex space situation, the threat index analysis model is able to predict the threat of actively approaching spacecraft so as to take timely protective measures and improve the survivability of satellites.

    AIR SPACE DEFENSE SYSTEM AND WEAPON
    Analysis of the Sixth Generation Fighter Development and Operational Concept
    Bao-jun ZHAO, Shi-tao CHEN, Da-xi LI, Ran ZHAO
    2022, 50(6):  19-25.  doi:10.3969/j.issn.1009-086x.2022.06.003
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    In order to identify the potential threat of the next generation fighter to the air defense system, the sixth generation fighter development plans and progress about US, Japan, UK, and French are analyzed. The typical capability characteristics and requires are identified, and the typical operational concepts are analyzed. The typical operational modes are identified initially, and it will provide the reference of the threat drive and development direction traction for the ground-based air defense system.

    Research on Anti-missile Operation Organization and Operation Application of Russian Army
    Jia-le GAO, Yi-zeng WANG, Dong-ya LIU, Jian GUO
    2022, 50(6):  26-34.  doi:10.3969/j.issn.1009-086x.2022.06.004
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    The development of Russia's anti-missile system used to lead the world, but it was also delayed by institutional reform. Its existing gradually mature anti-missile system construction, development and application of ideas for the construction of our military anti-missile system is of great significance. The Russian anti-missile system is analyzed from four aspects of the operation organization, equipment composition, force employment and use strategy. Firstly, the anti-missile operation system and mechanism of Russian army are analyzed from strategic and non-strategic perspectives. Secondly, the basic performance of command and control, early warning detection and fire interception system of Russian military anti-missile equipment is introduced. Finally, the strategy of using anti-missile combat forces is summarized, and some suggestions on the development of China's anti-missile combat system are put forward.

    AIRCRAFT TECHNOLOGY
    Analysis on the Development and the Potential Military Application of American Combined Propulsion Technology
    Yan-hua BIE, Bing-xuan LIN, Hang-yi SUN, Ming-xing XU, Yan-ming SHEN
    2022, 50(6):  35-41.  doi:10.3969/j.issn.1009-086x.2022.06.005
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    As an ideal propulsion system for hypersonic flight in near space and wide speed range and large airspace flight of aerospace vehicles, the combined propulsion system has high aviation and aerospace application value. Based on the analysis of the current combined propulsion schemes in the United States, this paper makes a preliminary discussion and estimate on its technical development and trend. The potential military applications are analyzed by taking several typical combined power aircraft as examples. Some suggestions for the development of combined propulsion system in China are proposed.

    A Design Method of Rigid-Flexible Electrical Connection Assembly with Fuzz Button Connector
    Yu-xin CHEN, Yu-tian CHEN, Hai-bo TANG, Fan-zhuo MENG, Yang GAO
    2022, 50(6):  42-49.  doi:10.3969/j.issn.1009-086x.2022.06.006
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    The electrical connection of each device inside the ultra-micro aerial vehicle(UMAV), mainly relies on the traditional way of lead wire welding. There are many problems in this way, such as low efficiency, error-prone, easy to broken welding wire, difficult debugging, etc. Ordinary wire-type cables and connectors are easy to use, but too bulky to suit the UMAV. A design method of fuzz button flexible electrical connection component for UMAV is proposed. The fuzz button component is used as the connector, the rigid-flexible joint plate is used as the transmission cable, and the three-dimensional design of aircraft structure is combined to realize the reliable electrical connection of various electrical devices inside the UMAV.

    NAVIGATION,GUIDANCE AND CONTROL
    Application of Data-Free Intelligent Technology in the Transfer Alignment of Maneuver Concomitant Anti-aircraft
    Ying HE, Jia-qing WAN, Shan-shan WEI, Xiao-qiang HU
    2022, 50(6):  50-58.  doi:10.3969/j.issn.1009-086x.2022.06.007
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    Due to the particularity of the application scenarios of maneuver concomitant anti-aircraft weapon systems, it is difficult to accurately establish a flexural deformation model that adapts to changing working conditions, and the accuracy of transfer alignment cannot be guaranteed. To solve this problem, a data-free intelligent technology is adopted, and the flexural deformation model in the transfer alignment mathematical model is replaced by a neural network. The connection weight coefficients of the neural network are expanded to part of the unknown variables of the transfer alignment model. The nonlinear Kalman filter is used to estimate all the variables of the model in real time, so as to obtain the misalignment angle between the main and the sub-inertial navigation. Based on the attitude information of the main inertial navigation system, the high-precision speed alignment during the movement is completed. Simulation experiments show that this method can estimate the misalignment angle in a short time and complete the high-precision initial attitude binding of the missile inertial navigation system.

    Research on Space-Based Information Subscription and Distribution Service for Long-Range Precision Strike
    Shu-rui ZHANG, Fan-de YANG
    2022, 50(6):  59-67.  doi:10.3969/j.issn.1009-086x.2022.06.008
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    The application of space-based information is an important foothold in the development of aerospace construction. In view of the rapid improvement of space-based information service capabilities to meet the changing objective needs of future operations, and the background of long-range precision strikes in the typical combat mode of modern warfare is used as the background of space-based information services, and the long-range precision strike combat process is analyzed. A conceptual model of space-based information and battlefield elements in long-range precision strike operations is constructed, combined with the model and referred to the principle of semantic-based publish-subscribe system, a multi-layer index structure for subscription requirements is proposed to realize long-range precision strikes subscription and distribution of space-based information in operations, and finally the performance of the method is verified to meet the operational requirements by experiments.

    COMMAND CONTROL AND COMMUNICATION
    Improved Evolutionary Decision Tree for BVR Air Combat Decision Making
    An XU, Wan-ze ZHENG, Zhi-fei XI, Lu-fei DANG
    2022, 50(6):  68-82.  doi:10.3969/j.issn.1009-086x.2022.06.009
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    Aiming at the decision-making problem of beyond visual range (BVR) air combat, a decision rule tree model that integrates prior knowledge of tactical implementation distance with evolutionary iteration capabilities is established. The mechanism of air combat victory is analyzed, the BVR air combat situation model and the tactical implementation distance model are established, the BVR air combat factors are introduced and the posture assessment model and the set of decision variables are established; the BVR air combat tactical action decomposition and the construction of the action library are implemented; the BVR air combat Decision tree are established, a new particle swarm optimization method based on dynamic adjustment of inertia weights and chaotic optimization is proposed to improve the evolution efficiency realization of the decision rule tree; based on the simulation experiment, the decision effect analysis of the evolutionary decision tree under different conditions is given. The simulation results show that the evolutionary decision tree proposed can effectively integrate a priori knowledge of tactical implementation distance, missile strike zone, etc., and has the evolutionary capability to effectively solve the BVR tactical decision problem.

    TARGET CHARACTERISTIC, DETECTION AND TRACKING TECHNOLOGY
    Range Walk Analysis and Compensation Algorithm of Interrupted Continuous Wave Dechirp System
    Xue-zhen JIA, Wu SUN, Qiu-feng XU, Rui-rong CHEN
    2022, 50(6):  83-89.  doi:10.3969/j.issn.1009-086x.2022.06.010
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    The paper makes a quantitative analysis on the range walk of high-speed target and its influence on signal-to-noise ratio in interrupted continuous wave dechirp system. The analysis results show that the difference frequency signal when range walk occurs is a LFM(linear frequency modulation) signal. Aiming at this phenomenon, a time-domain inversion compression compensation method is proposed, which uses the time-frequency characteristics of the signal to generate a time-reversed signal in the time domain, which is conjugated and multiplied with the original signal to remove the frequency modulation slope and realize signal compression. At the same time, a quadratic matched filter compression method is proposed. Based on the speed search information, the frequency modulation slope of the difference frequency signal during range walking is calculated, and the matched filter with the opposite slope is generated. The range walking is eliminated by quadratic matched filtering. It can eliminate the influence of distance walking of high-speed targets, improve the detection power and detection accuracy, and can be applied to the declination system interrupt CW detection radar, which has a good reference significance in the field of high-speed target detection.

    Study of Full-Polarization Interference Modulation on Polarization Filter of Array Radar
    Xiao-wen ZHANG, Qiang WANG, Zhi-mei HAO
    2022, 50(6):  90-96.  doi:10.3969/j.issn.1009-086x.2022.06.011
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    Owing to the lack of polarization freedom and the power-driven, the polarization filter cannot meet the demand of setting notch at the interference and setting peak at the target simultaneously. This disadvantage is considered as the fundamental of corrupting filter. The jammer can prevent the radar from obtaining the precise target, interference polarization parameters and stable related interference and noise reference data necessary for the filter by controlling the mode and sequence of polarization of the transmit signal polarization modulation, which in turn prevents the filter notch from aligning with the interference and ensures that sufficient interference signal is received by radar receiver. We analyze the processing characteristics of various polarization filters and predict the filter output performance for various interference backgrounds to obtain the best polarization modulation scheme against each filter. The schemes are verified by simulation experiments.

    Frequency Shift Interference Suppression Method Based on Frequency Estimation and Signal Reconstruction
    Shan-shan JIN, Xin LI, Chen LIU
    2022, 50(6):  97-102.  doi:10.3969/j.issn.1009-086x.2022.06.012
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    Frequency shift interference can produce high fidelity false targets for the range-Doppler coupling characteristic of LFM signal. According to the peak characteristics of pulse echo by compression and the principle of dechirp, the interference suppression method based on signal reconstruction and cancellation is proposed. Firstly, the frequency of the signal by dechirp is estimated, and the dechirp interference signal is reconstructed. Secondly, the normalized average detection threshold is defined for the dechirp signal, and the minimum threshold is used as the objective function of interference suppression. Finally, the interference suppression factors corresponding to the minimum normalized average monitoring threshold are calculated by global search, and interference suppression is realized by cancellation. The simulation shows that the energy of residual interference component is more than 20 dB lower than that of target echo in the output signals by pulse compression, which shows the proposed method can suppress multi-frequency shift interference effectively.

    INTEGRATED LOGISTICS SUPPORT TECHNOLOGY
    Software Reliability Evaluation Method Based on Component Importance
    Ying-bo LI, Li-li TAN, Kai-xuan WANG, Zhuo LIANG, Yan-peng PAN
    2022, 50(6):  103-109.  doi:10.3969/j.issn.1009-086x.2022.06.013
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    The software reliability of component-based development depends on component reliability,but component reliability is affected by test coverage and usage frequency.Therefore,the reliability evaluation of new components is often low.When a newly developed component is introduced into mature software,no matter the importance of component,the software reliability evaluation value will change greatly.To solve this problem,taking a software as the research object, a Markov chain software model based on functional scenario is established. the importance of each component in the model is evaluated by analytic hierarchy process.On this basis,a software reliability evaluation model based on component importance is established.The simulation results show that the model can more accurately reflect the software reliability level of component-based development.

    Missile Equipment Quality Condition Assessment Under Fuzzy Evaluation Grade
    Yao LEI, Jian-yin ZHAO, Yu BAI
    2022, 50(6):  110-116.  doi:10.3969/j.issn.1009-086x.2022.06.014
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    This paper aims to use the method of evidential reasoning (ER) algorithm based on fuzzy uncertainty to provide the basis for missile quality condition assessment, especially to deal with many unquantifiable factors, as well as factors which are inaccurate, unclear and incomplete. The ER algorithm operates in a system where both unknown and fuzzy data are modeled under the unified framework of distributed fuzzy belief structure to form a fuzzy belief decision matrix. Using the grade matching method, the numerical data and various forms of qualitative (fuzzy) evaluation information are finally transformed into fuzzy belief structure. This method can fuse the evaluation levels of important parameters without iteration on the premise of maintaining the independence with fast degradation speed, so as to improve the sensitivity and applicability of the evaluation process.

    Scheduling of Special Support Vehicles at Naval Aviation Station with Time Windows
    Zhe YAN, Min-le WANG, Jiang-peng WANG, Feng-xuan WU, Shao-qiang YAN
    2022, 50(6):  117-123.  doi:10.3969/j.issn.1009-086x.2022.06.015
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    With the dramatic increase in the style and number of naval aviation missions, the experience-based manual scheduling type of special support vehicle dispatching method will not only cause a waste of support resources, but also easily lead to delays in warplanes due to untimely dispatch of vehicles. To address the problem of dispatching special support vehicles at naval aviation station, a mathematical model is established with the objective of dispatching the least number of support vehicles and the shortest total vehicle travel distance under the constraints of time window and vehicle load. The model is solved by improving the initial population and coding method of genetic algorithm, and a simulation test is carried out with a multi-aircraft and high-volume flight protection task to obtain a special support vehicle dispatching scheme, which verifies the rationality of the model.

    SIMULATION TECHNOLOGY
    An Improved UAV Low Altitude Penetration Model Based on Safe Flight Space
    Ping YANG, Shao-qiang YAN, Jiang-peng WANG, Feng-xuan WU, Zhe YAN, Song YAN
    2022, 50(6):  124-131.  doi:10.3969/j.issn.1009-086x.2022.06.016
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    An improved unmanned aerial vehicle (UAV) low altitude penetration model based on safe flight space is presented to solve the problem of lack of combination with the characteristics of UAV after terrain preprocessing. A safe flight space is constructed to reduce terrain constraints and ensure the safe flight of UAV in low altitude penetration. The trajectory planning model is improved by combining with the characteristics of UAV to increase the stability of UAV flight process and the smoothness of planned trajectory. The particle swarm optimization (PSO) algorithm is used to simulate the two models before and after the improvement in complex elevation map to verify the rationality and effectiveness of the improved model.

    Review of Simulation and Experimental Research on Gas Rudder Complex Environment
    Rui-ze DU, Hou-xin HE, Yong-li LIU
    2022, 50(6):  132-140.  doi:10.3969/j.issn.1009-086x.2022.06.017
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    As one of the missile thrust vector substitution control schemes, the gas rudder operates in a very complex high-temperature gas environment. It is difficult to accurately predict the surface force and thermal load of the gas rudder and predict its ablation. At home and abroad, relevant researches have been carried out on the aerodynamic characteristics and related thermal environment of gas rudders through experiments and numerical calculations, which proves the feasibility and accuracy of predicting and simulating gas rudder ablation by numerical method, and provides strong support for the subsequent design and optimization of gas rudder in engineering practice.