Simulation And Study Of Fighter Launch Air-to-Air Missile Guided By AWACS

At present, the philosophy of military combat has already changed a lot with the development of military technology. The characteristics of high-tech related wars in modern days will soon become information wars, which require all kinds of information should be simultaneously shared and well coordinated in the battle field. AWACS has plenty of functions such as alarming, commanding control, communication as well as electronic warfare, etc., and it also serves as the radar station and command center in the air. The basic philosophy of modern military combat is: AWACS detects an aerial target and guides fighters to attack it.The use of AWACS technology to command fighters to attack a target has already been applied to actual fights in the air, and the related theory and researches have already became pretty mature. However, the studies in this field started quite late in China, and thus its technologies was rather backward. Therefore, the present research was concerned with principium study and simulation of fighter launch air-to-air missile guided by AWACS.The main contents in this study are as follows:Firstly, the study analyzed the cruise route of AWACS, and built the corresponding mathematic mode, and then simulated double parallel cruise route. In addition, it expounded the constitutes, functions and development of the system, and it also transferred information of target which detected by AWACS radar to fighter.Secondly, it analyzed two processes of close navigation and remote navigation of fighter attack target guided by AWACS, and it simulated pure proportion guidance and pure collision attack in the long distance. Further more, it detruded optimum guidance of time, realized least time and least energy guidance. In the close guidance process, it adopted matrix countermeasure law and the analogy proportion law to realize the best advantage place of fighter.Thirdly, it studied midcourse guidance laws and end guidance laws of air-to-air missile. The optimum forecast proportion guidance was detruded in the midcourse guidance process. Based on the optimization control theory, it detruded a modulus proportion guidance law of end guidance process.Finally, the thesis adopted the idea of modularization design to divide the processes of fighter launch air-to-air missile into some main-modularizations and some sub-modularizations, and at the same time simulated the processes of AWACS,...