基于GPS的仪表着陆系统飞行检验建模  

The Modeling of Instrument Landing System Flight Inspection Based on Global Positioning System

作　　者：刘勇[1] 武昌[1] 陈校平[1] 段亚军[1] 

机构地区：[1]空军工程大学电讯工程学院,陕西西安710077

出　　处：《空军工程大学学报（自然科学版）》2006年第4期20-22,共3页Journal of Air Force Engineering University(Natural Science Edition)

基　　金：军队科研基金资助项目

摘　　要：GPS是新一代卫星导航与定位系统,它定位精度高,具备提供多维的时空位置速度信息及连续导航能力。文中根据GPS定位原理、飞行动力学理论及仪表着陆系统信号体制,建立了以GPS作为基准系统的ILS飞行检验模型,为进一步的研究提供指导。Global Positioning System is a new generation satellite navigation and positioning system. This can provide fine precision, multi - dimensional space - time position and velocity information. According to the positioning principle of Global Positioning System, the theory of flight dynamics and the signal system of Instrument Landing System, this paper builds up a model of the Instrument Landing System flight inspection, in which the Global Positioning System is adopted as a benchmark system in order to direct the further research.

关 键 词：全球定位系统 仪表着陆系统 飞行检验 建模 

分 类 号：V351[航空宇航科学与技术—人机与环境工程]