制导应用的逼真导弹建模

M. Sobh, M. Sheirah
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引用次数: 5

摘要

本文提出了一种通用的导弹建模方法。提出了一种考虑六自由度三维空间刚体动力学的精确导弹模型。还考虑了不同的坐标系、导弹质量变化、空气动力学、空气速度和密度、重力、推进系统、作动器、测量和跟踪装置。整个模型在仿真环境中实现和集成,以方便导弹制导设计。该模型具有较高的仿真速度和较好的计算精度。其他模块用于计算空气动力学系数,生成随机信号,提供常规和智能控制,并可视化地表示导弹与目标的交战。整个系统成功地实现了不同的制导技术
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Realistic Missile Modeling for Guidance Applications
In this paper, a general missile modeling is presented. An accurate model for missiles is proposed taking into consideration the rigid body dynamics in 3D space with 6 degrees of freedom. Different coordinate systems, variation of missile mass, aerodynamics, air speed and density, gravity, propulsion system, actuators, measurement and tracking devices are also considered. The full model is implemented and integrated within a simulation environment to facilitate missile guidance design. The developed model is optimized for both high simulation speed and accurate calculations. Other modules are implemented to calculate aerodynamics coefficients, generate random signal, provide both conventional and intelligent control, and represents the missile-target engagement visually. The whole system is successfully used to implement different guidance techniques
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