区域导航

基于必备导航性能的区域导航及其效益分析

Benefit Analysis of RNAV Based on RNP

区域导航航路和进离场程序设计分析与仿真

Analyzing and Simulating of RNAV Route and SID STAR Procedure Design

Walker星座的区域导航特性分析

Analysis of Area Navigation Performance of Walker Constellation

RNP区域导航技术，是利用飞机自身机载导航设备和全球定位系统引导飞机起降的新技术。

RNP regional airmanship refers to make use of aircraft self-carrier navigation equipment and the new technology channel off rise-and-down by GPS .

提出了一个由八颗同地迹有一定倾角的地球同步圆形轨道（IGSO）卫星组成的区域导航星座方案。

A regional navigation constellation scheme composing eight IGSO satellites of ground track is presented in this paper .

为提高RNAV（区域导航）精度，采用空间向量分析，导出了FANS（国际民航组织倡导的新航行系统）航线的初始航线角和航线距离计算公式；

To improve the precision of area navigation , the formulas of calculating the initial course and route distance of an FANS ( the future air navigation system ) route was derived through spatial vector analyses .

圆轨道同步卫星在区域导航系统中应用研究

Application Analysis of Circle Orbit Synchronous Satellite in Regional Navigation System

区域导航星座分析设计研究

Studies on the Design and Analysis of Regional Navigation Constellations

一种新的中国区域导航系统星座方案的探讨

Research on a New Constellation of Regional Satellite Navigation System Covering China

基于DME/DME的区域导航航路导航性能评估方法

Assessment Method of RNAV Route Based on DME / DME

近空间区域导航增强系统信号设计与验证

Signal Design and Validation of the Near Space Local Area Augmentation System

直扩体制区域导航系统的定位精度分析

Analyse on Positioning Precision in Area Navigation System Based on DS Spread Spectrum

我国区域导航航路和进离场程序设计方法研究

Study on the Methods of Chinese RNAV Route and Sid Star Procedure Design

平行区域导航航路安全性分析

Security Analysis of Area Navigation Parallel Airway

亚太区域导航八星星座分析

The Analysis of Regional Navigation Constellation

并对该方案进行了仿真验证，研究了低轨道航天器区域导航的轨道预报效果。

Then the program is simulated in order to study the effect of the low-orbit spacecraft orbit prediction .

防止非用户启动一个区域导航到一个较高的安全地带页页之间。

Prevent non-user initiated navigation between a page in one zone to a page in a higher security zone .

本论文推导了区域导航定位系统的几何精度因子，并用矩阵理论对其最小值及其随导航台个数增加而减小进行了证明。

In this paper , the GDOP ( geometric dilution of precision ) expression of area navigation system is deduced .

其次，研究了基于VOR/DME导航台的区域导航飞行程序的设计方法；

Secondly , this thesis investigates the designing methods for VOR / DME-based area navigation flight procedure ( RNAV FP ) .

在区域导航定位系统中，假设导航台和用户都在同一水平面。

In the area navigation system , we may suppose all of navigation stations and the users on the same horizontal level .

飞行管理系统是区域导航系统和性能管理系统的高度综合，其核心问题就是优化飞行轨迹的生成和实现。

FMS whose key questions are generation and realization of optimum flight trajectories are synthesized by area navigation systems and performance management systems .

这篇论文是首次较全面研究国内外区域导航飞行程序设计标准、方法和实施情况。

This article study the RNAV procedures design criteria , method and implement in China and abroad more generally for the first time .

通过仿真结果反映了飞行计划管理系统功能完备、性能良好、操作简单、满足区域导航要求。

The verification result represents that the flight plan management system is fully functional , has a good performance and simple operation , and meets the requirements of RNAV .

针对区域导航星座扩展性能要求进行了基于基准构型的区域导航星座扩充优化设计。

In view of the expansion performance requirements of the regional navigation constellation , the expansion optimization design of the regional navigation constellation based on the basic configuration is carried on .

本文着重介绍战术飞行管理系统的概念、要求和展望。战术飞行管理系统是最近才提出的区域导航、能量管理、突防、地形跟踪/回避、提高机动武器效能的综合系统概念。

A Tactical Flight Management ( TFM ) system has been developed that incorporates system concepts for enroute navigation , energy management , threat penetration , terrain following / terrain avoidance , and advanced maneuvering weapon delivery .

区域导航是一种可以使飞机在任何定义的或合适的飞行路线上运行的导航方式，易于建立直飞航路，平行航路和旁通航路，提高了导航精度。

Aera Navigation ( RNAV ) is a navigation mode that enable airplane to operate in any defined or proper route . It 's easy to establish direct route , parallel route and bypass route , enhance navigation accuracy .

结合航空仿真技术发展和全任务飞行模拟器样机的任务需求，在MATLAB/SIMULINK平台上构建了捷联惯导及基于区域导航法的无线电导航仿真模型。

Considering current development of aviation simulation technology and practical request of the prototyping of full flight simulator , strap-down inertial navigation model and radio navigation models with the method of region navigation were made on MATLAB / SIMULINK platform .

随着区域导航和所需导航性能的实施，平行航路、随机航路和起点和终点之间的大圆航线直飞得以实现，提高了空域利用率和飞行安全。

With the application of area navigation and Required Navigation Performance ( RNP ), this would make the parallel route , random route and direct flight route possible , and also improves the efficiency of air space and the flight safety .

本论文分析了基于直扩的区域无线电导航系统的总体结构和工作原理，对区域导航中和定位精度有关的部分进行了研究，并利用matlab软件进行建模仿真。

This thesis analyzes the principle and architecture of area navigation system and investigates the problems related with positioning precision , which are modeled and realized with simulation tool , Matlab .

对终端区域4D导航中高度剖面和速度剖面生成的基本算法进行了研究。

An algorithm to realize the altitude profile and speed profile of 4D guidance in terminal area is presented in this paper .