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作 者:武文峰[1] 龚铮[1] Wu Wenfeng;Gong Zheng(China Air-borne Missile Academy,Luoyang Henan,471009)
出 处:《电子测试》2020年第7期133-134,共2页Electronic Test
基 金:航空科学基金资助(20160112002)。
摘 要:现有制导控制系统设计开发平台的技术复杂性与快速开发之间形成了突出的矛盾,而且普遍存在设计平台维护成本高、扩展性差等一系列问题。针对以上问题,建立了导弹制导控制系统的各个子模型,研发了导弹制导控制系统设计平台。平台将视景仿真功能与数字仿真功能相结合,建立制导控制系统仿真环境,并将导弹仿真数据进行实时显示及结果复现,用三维动画图像的方式,来展示导弹弹道轨迹、位置姿态、自身状态、传感器覆盖范围等,对目标识别、弹着点预测、引战配合攻击效果评估等分析结果进行可视化,更清晰地描述出制导控制系统的实时运行状态,在提高导弹制导控制系统设计性能和质量等方面具有积极的意义。The technical complexity and rapid development of existing guidance and control system design and development platforms have formed prominent contradictions,and a series of problems such as high maintenance costs and poor scalability of design platforms are common.In response to the above problems,each sub-model of the missile guidance control system was established,and a missile guidance control system design platform was developed.The platform combines the visual simulation function with the digital simulation function,establishes a guidance control system simulation environment,and displays the missile simulation data in real time and reproduces the results.The three-dimensional animation image is used to display the missile trajectory,position and attitude,and itself Status,sensor coverage,etc.,to visualize analysis results such as target recognition,impact point prediction,and piloting with attack effect evaluation,to more clearly describe the real-time operating status of the guidance control system,and to improve the design performance and quality of the missile guidance control system.Aspect has a positive meaning.
分 类 号:TJ765[兵器科学与技术—武器系统与运用工程]
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