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Simulation Research on Equipment Battlefield Repair Based on ExtendSim Platform
Xuguang TIAN, Longtao WU, Chengming ZHANG, Qinwen ZUO, Ning LIU
Modern Defense Technology    2025, 53 (3): 191-199.   DOI: 10.3969/j.issn.1009-086x.2025.03.022
Abstract2)   HTML0)    PDF (1803KB)(1)       Save

This paper constructs a simulation model for the equipment battlefield repair process under the ExtendSim simulation platform to study the impact of various maintenance support resource elements in the equipment battlefield repair process. A conceptual model of the equipment battlefield repair process was constructed; the modeling boundary was analyzed and a simulation model based on ExtendSim was constructed. On this basis, simulation was conducted on the battlefield repair process of equipment. Through analysis, it is believed that under certain simulation conditions, there is an optimal number of testing personnel and equipment, which results in relatively stable equipment utilization, support personnel utilization, task waiting time, and average task completion time, without consuming excessive maintenance resources. When the number of inspection personnel and equipment is too small, the simulation system runs extremely unstable, sometimes even unable to complete the simulation process. Conversely, an excessive number of inspection personnel and equipment does not significantly improve maintenance efficiency. The impact of equipment heavy-damage rates on the repair process is also studied. The research results of this article aim to provide technical support for the organizational decision-making process of equipment battlefield repair.

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Arithmetic on Guidance and Control for Hyper Velocity Kinetic Energy Missile Based on Sliding-Mode Variable Structure Control
Si-yang JIAO, Tao PAN, Zhe KONG, Bao-Ning LIU
Modern Defense Technology    2022, 50 (2): 53-60.   DOI: 10.3969/j.issn.1009-086x.2022.02.008
Abstract2941)   HTML71)    PDF (1809KB)(644)       Save

A guidance and control arithmetic of hyper velocity kinetic energy missile is designed based on sliding-mode variable structure control. The relevant parameters in the algorithm are designed and adjusted by combining the characteristics of the hyper-velocity kinetic energy missile and the operational mission requirements. The algorithm is used to suppress the chattering problem inherent in the control of sliding mode variable structure, and the modeling simulation confirms the correctness and feasibility of the algorithm. According to the analysis of the simulation results, the hyper-velocity kinetic energy missile can hit its target because of the guidance and control arithmetic, and the processed chattering of sliding mode control can be suppressed.

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