Aero Weaponry

The conception of ultra-tight integrated GPS /INS navigation system is introduced.According to the variation of architectures and information processing methods,the ultra-tight GPS / INS integrated navigation system can be classified into three modes,which are INS aided ultra-tight integration,coherent deep integration and non-coherent deep integration.On the basis of providing architectures of different ultra-tight integration modes,their features are compared and analyzed respectively.The developments of GPS / INS ultra-tight integration at home and abroad are reviewed,and the key technologies and future directions of ultra-tight integration are pointed.

Wang Xin-long

Hangkong bingqi

Survey of GPS/INS Ultra-Tight Integrated Navigation System

GPS/INS超紧耦合导航系统综述

A digital servo control system design of a certain air-to-air missile based on DSP is proposed.Composing principle,the hardware design and control algorithm are described.Compared with analog circuit controller,the digital controller has characteristics of modifying parameter conveniently and good control precision and good anti-jamming ability.Experimental results show that the controller has good static characteristics and dynamic characteristics.

Liu Peng

Digital Servo Control System for Air-to-Air Missile Based on DSP

基于DSP的空对空导弹数字伺服控制系统

In order to improve the synthetical performance of fluidic thrust-vectoring nozzle working at high nozzle pressure ratios(NPR),a design concept of a high NPR fluidic thrust-vectoring nozzle is proposed based on dual-throat thrust-vectoring nozzle,and numerical simulations are conducted to investigate the flow characteristics and the effects of key design parameters on nozzle performances.Results show that the proposed design in this paper has a higher synthetical fluidic performance.

Tan Hui-jun

Simulation Study of a High NPR Fluidic Thrust-Vectoring Nozzle

高NPR射流推力矢量喷管的仿真研究

The wireless channel simulation model of airborne missile data link is the basis of the data link scheme design and the algorithm validation.This article analyzes the wireless channel transmit characteristics of aeronautical communication and establishes the data link model based on the delay taps model.Compared the simulation with result of the literature data,the validity of the simulation model is confirmed.

DU Xiang-hu

The Study of Airborne Missile Data Link Channel Model

机载导弹数据链通道模型研究

Phased array radar seeker is a new radar seeker which uses advanced phased array antenna technology.Compared with conventional radar seeker,this seeker offers a number of attractive features.This paper presents its development and recent progresses,analyses its technical characteristics and difficulties,and gives the future development direction.

LI Chao-wei

Summarization of Phased Array Radar Seeker

相控阵雷达导引头综述

Opto electronic servo control software( OESCS) is an important component of the optoelectronic stabilized platform,engineers pay more and more attention to the debugging problem. This paper starts from the analysis of the characteristics of OESCS,the problems of OESCS'debugging process which is difficult to solve by using traditional method are stated. According to these problems,the specialistic debugging tool for OESCS is designed. The function demand and design essentials are discussed,and the top framework of debugging tool is constructed using the modular programming idea.

Liao Hong-b

The Top Framework Design and Application of Debugging Tool for Opto Electronic Servo Control Software

光电伺服控制软件调试工具的顶层框架设计与应用

Based on analyzing the structure composition of air-to-air missile,referring to the open system architecture for condition-based maintenance( OSA-CBM),the PHM frame model for air-to-air missile is put forward and two case study applying PHM technology on air-to-air missile in service are carried out. By analyzing the factors influencing the performance of missile in store,the parameters needed are determined,requirements on choosing sensor systems according to its cost,shape and transmission mode are given,and condition monitoring system for missile package box is established. Using the parameters adopted in electrical characteristic test and the theory of setting parameter ranges,scoring criteria is set up,and the state indexes of missile is accumulated with weight.

LI Zhi-qian

Research on Architectural Design of PHM System for Air-to-Air Missile

空空导弹PHM系统架构设计研究

During the laser ranging,the error caused by time-interval measurement error can produce when the pulse width of laser fuze is too wide. So a new range finder method for pulse laser fuze is proposed. The method is first measuring the delay time of transmitted pulse signal and return pulse signal through real-time detecting the center of echo waveform,and then calculating the target range with it. Appling this method a series of range experiments are proceeded,the experimental data are given and the error is analyzed in theory. The results show that the precision of 0. 5 m level is achieved and the ranging precision of the laser fuze is improved,which meets the practical needs.

Li Jin

A Range Finder Method for Pulse Laser Fuze Based on the Center of Echo Waveform

基于回波波形中心的脉冲激光引信测距方法

In order to lower effectively the technical risk of weapon research development,the American Department of Defense( DOD) adopted the notion of Technology Readiness Level( TRL) as well as Technology Readiness Assessment( TRA),and continuously expanded their application field and scope to improve and develop the notion of System Readiness Level( SRL) as well as System Readiness Assessment( SRA). This article introduces the basic concept of TRL and TRA,and then further introduces the basic concept of SRL,SRA and a widely-used assessment method called Matrix-based Model,and applies the assessment method to the airborne guided weapon research development work as a practical instance,presenting an useful reference for TRA of domestic complex integrated systems.

Wang Fan

Application Research on Matrix-Based Model of System Readiness Assessment in Airborne Guided Weapon Research & Development

基于矩阵模型的机载制导武器系统准备度评估应用研究

The conception of acquisition techniques of high sensitivity GPS is introduced. According to the way of improving the sensitivity of GPS,the acquisition techniques of current high sensitivity GPS is classified into three modes,which are techniques of upgrading the SNR method,cross-correlation interference mitigation method and assisted GPS acquisition method. On the basis of analyzing the methods of high sensitivity GPS modes,their features are compared and analyzed respectively. The development of techniques of high sensitivity GPS at home and on abroad are reviewed. The key technologies and future trend of high sensitivity GPS acquisition techniques are pointed.

acBWQ6	AERO WEAPONRY
xGGr6y	北大核心中国科学引文数据库中国科技核心期刊目录

ISSN	1673-5048
h-index	11

u9zg3I	aviation weaponweaponry operationexperiment validationunmanned aerial vehicleguidance and counseling
+5d/bs	e+/GRg: Editorial Office of Aero Weaponry，uzYam8: ，dxwaWB: journal，8x2mMQ: Xn96QY
ak9yM6	A7IHrH: 2019，sQJ/D8: 0.00%，sE9og+:N.A.， wzlKC/: 0.00%
JrpmBe	网友分享经验：50 Weeks

Aero Weaponry

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Survey of GPS/INS Ultra-Tight Integrated Navigation System

Digital Servo Control System for Air-to-Air Missile Based on DSP

Simulation Study of a High NPR Fluidic Thrust-Vectoring Nozzle

The Study of Airborne Missile Data Link Channel Model

Summarization of Phased Array Radar Seeker

The Top Framework Design and Application of Debugging Tool for Opto Electronic Servo Control Software

Research on Architectural Design of PHM System for Air-to-Air Missile

A Range Finder Method for Pulse Laser Fuze Based on the Center of Echo Waveform

Application Research on Matrix-Based Model of System Readiness Assessment in Airborne Guided Weapon Research & Development

Review of Acquisition Techniques of High Sensitivity GPS