摘要
本文将飞行器随机动力学模型、干涉仪定位测速模型和多站联测的EMBET模型统一转化为离散时间的线性动态一测量系统模型，为飞行器外测系统的计算机仿真提供了统一的模型框架。
In this paper, three kinds of orbits - determination m0dels, including locationmodel using continuous - wave radar, the orbit -dynamic models and the EMBET model, areunified into the discrete timc dynamic & measurement systems. S0, much 0f the simulation~ can be done in a c0mmon framework.
出处
《电脑与信息技术》
1998年第4期24-27,33,共5页
Computer and Information Technology
关键词
飞行器
计算机仿真
外弹道测量系统
建模
Aircraft Trajectory and Orbit Measurement System Computer Simulation
