基于X-Plane的某巡飞弹快速原型及一体化建模

发布时间：2018-03-31 12:21

  本文选题：巡飞弹　切入点：X-Plane　出处：《系统仿真学报》2017年11期

【摘要】：针对巡飞弹前期设计验证过程中,数学建模及气动参数分析方法研发难道大、周期长等问题,提出采用X-Plane的快速原型及一体化建模方法。分析巡飞弹的特点并总结了各类仿真方法的运行机制,分析了X-Plane的原理;通过机体建模实现了巡飞弹不依赖于数学模型及气动参数的快速原型搭建,改进了翼型及桨叶设计,实现了特殊控制(混控、伞降及折叠翼);通过软件在回路仿真方法验证了飞行器设计及控制器性能。研究成果表明:该方法能够实现各类飞行器前期快速原型设计及验证,具有研发周期短,可视化效果好等特点,对飞行器设计及控制算法研究人员均有借鉴意义。
[Abstract]:In view of the problems of the research and development of mathematical modeling and aerodynamic parameter analysis methods in the verification process of the preliminary design of the cruise missile, such problems as the long period and so on, A rapid prototyping and integrated modeling method based on X-Plane is proposed. The characteristics of cruise missile are analyzed, the operation mechanism of various simulation methods is summarized, and the principle of X-Plane is analyzed. By modeling the airframe, the rapid prototyping of cruise missile independent of mathematical model and aerodynamic parameters is realized, and the airfoil and blade design are improved, and the special control (mixed control) is realized. The performance of aircraft design and controller is verified by software in loop simulation. The research results show that this method can realize the rapid prototyping design and verification of all kinds of aircraft, and has a short research and development period. The visualization effect is good, which can be used for reference by researchers of aircraft design and control algorithm.
【作者单位】： 西北核技术研究所;军械工程学院无人机工程系;
【分类号】：TJ410;TP391.9
，

本文编号：1690714