飞机导航系统

某型飞机导航系统惯导校正方式研究

Research of Inertial Navigation Correction Modes in a Aircraft Navigation System

本文的研究，为该型飞机导航系统校正方式控制率的改进研制，提供了相应的理论支持。

This paper will provide the corresponding theoretical support for domestic development of correction mode control ratio in aircraft navigation systems .

该项研究已纳入国家某工程型号任务之中，对提高飞机导航系统精度及飞控与火控系统性能有重要意义。

The research is already brought into a type of project , and it has important significance in improving precision of airplane navigation system and capabilities of flight control system and firepower control system .

采用这种实时多任务软件结构，能够有效地降低软件设计的复杂度，显著提高导航系统软件的可靠性、实时性和运行效率，满足了现代飞机导航系统发展的需要。

Using this software structure based on real-time multitask can significantly decrease the complexity of software design , and improve the reliability , real-time and operation efficiency of navigation software , hence can meet the needs of the development of modern navigation system .

无人驾驶飞机GPS导航系统的设计与实现

Design and Implementation of a Navigation System for Pilotless Aircraft Using GPS

某型飞机惯性导航系统校正研究

Study about Correct of INS of a Type of Airplane

某型飞机惯性导航系统模拟器软件设计

Software Design of an Airplane Inertial Guidance System Simulator

测距系统是飞机无线电导航系统的重要组成部分。

The distance measuring system is the important part of the navigation for the airplane .

一种飞机综合导航系统的研究

Research on an Airborne Integrated Navigation System

请关掉所有移动电话，因为他们会干扰飞机的导航系统。

Please switch off all mobile phones , since they can interfere with the aircraft 's navigation systems .

本论文主要是研究卡尔曼滤波参数混合技术应用于民用飞机相对导航系统。

This paper discusses mainly the technique of parameter hybrid of Kalman filter applied in the system of relative navigation .

轨迹测量源于惯性测量，是在飞机惯性导航系统的基础上发展起来的。而惯性导航是一种完全自助式导航。

Trajectory measurements comes from the inertial measurement which is based on the aircraft inertial navigation system and also is a completely self-navigation .

飞机图像导航数据库系统的设计与开发

The Design and Development of the Image Navigation Database for Airplane

飞机导航数据仿真系统设计

The Design of an Aircraft Navigation Data Simulator System

飞机加装组合导航系统方案

Programs for Adding Integrated Navigation System on Aircraft

机械学工程将这些原理应用于现实生活来处理核反应堆，混合动力汽车，实验性飞机，导弹导航系统等各种问题。

Engineering mechanics applies these principles to real-world design problems as diverse as nuclear reactors , hybrid automobiles , experimental aircraft , and missile guidance systems .

飞机自动着陆GPS导航系统采用差分法消除基准站和飞机接收机的GPS误差。

The GPS error of datum-station and airplane receiver was eliminated with difference method in GPS-navigating system for airplane automatic landing .

飞机导航设备自动测试系统飞机电缆敷设

The Automatic Testing System for Airplane Navigation Equipment Cable Arrangement in an Aircraft