基于高速飞行器火力控制模型的智能解算方法  

Intelligent solution method based on high-speed aircraft fire control model

作　　者：杨犇 金飞腾 刘燕斌 陈柏屹 彭寿勇 YANG Ben;JIN Feiteng;LIU Yanbin;CHEN Boyi;PENG Shouyong(College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China;College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China;Beijing Aerospace Technology Institute,Beijing 100074,China)

机构地区：[1]南京航空航天大学航天学院,南京211106 [2]南京航空航天大学自动化学院,南京211106 [3]北京空天技术研究所,北京100074

出　　处：《北京航空航天大学学报》2024年第5期1693-1701,共9页Journal of Beijing University of Aeronautics and Astronautics

基　　金：中央高校基本科研业务费专项资金(NS2021061);江苏省基础研究计划青年基金项目(BK20200437)。

摘　　要：研究吸气式高速飞行器的火力控制解算问题,针对高速飞行器较传统的亚音速与超音速飞行器系统响应时间短,飞行环境复杂,对火力控制模型解算要求度高等难点,提出了一种高速飞行器火力控制模型的解算方法。构建了面向高速飞行器平台的火力控制模型,并根据高速飞行器的飞行特性,使用快速模拟法结合阿基米德优化算法求解攻击区域,并反解出载机初始的指令信号。仿真结果表明,该解算方法解算精度高,控制参数少,所实现的攻击区域广,且能发挥高速飞行器较强的飞行性能。This paper studies the fire control calculation problem of air-breathing high-speed aircraft.High-speed aircraft has higher requirements for the fire control model calculation,a more complicated flying environment,and a shorter response time than traditional subsonic and supersonic combat aircraft.A calculation method of the high-speed aircraft fire control model is proposed.First of all,the mathematical model of the air-breathing high-speed flight vehicle is established;and the fire control model of the high-speed aircraft platform is constructed.Then,the attack area is solved using the fast simulation method in conjunction with the Archimedes optimization algorithm based on the flight characteristics of the high-speed aircraft,and the carrier aircraft's initial command signal is solved in reverse.The simulation results show that the solution method has high solution accuracy,few control parameters,wide attack area,and can exert strong flight performance of high-speed aircraft.

关 键 词：高速飞行器 火力控制 攻击区域 阿基米德优化算法 智能解算 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计] TB553[理学—物理]