空中加受油仿真中关键技术的研究

Study on Key Techniques about Refueling Simulation in Air

在某型军机空中加受油仿真成功研制的基础上,主要对加受油仿真中的4个关键技术进行了研究,通过对各种视景仿真技术特性的分析找到了适用于加受油仿真的最佳视景仿真解决方案,对尾流扰动特性、增稳特性进行了深入的理论研究,结合工程经验建立了尾流扰动模型和增稳模型,通过对系统实时性的分析,从多方面解决了加油机抖动的难题,达到了预期效果。

The four key techniques of refueling flight simulation are studied on the base of a modern avion effective refueling flight simulation in the air. Characteristic of the usual scene simulation techniques is analyzed and the best scene simulation solution is found out, the theories of vortex interference and control & stability are explored deeply, and the models of vortex interference and control & stability are built with engineer data, system real time performance is researched, and the irregular back and fro of the refueling plane is worked off. the ideal result is harvested.