摘要
针对飞行模拟机的燃油系统进行研究。分析燃油系统的工作原理,基于液体动力学计算燃油系统参数,使用C语言建立各分系统模型,将燃油系统模型接入飞行仿真实验系统,对燃油系统进行ATG测试。结果表明,建立的模型能达到使用要求。
Study on fuel system of flight simulator was carried out. The operational principle of the fuel system was analyzed. The parameters of the fuel system were calculated based on hydrokinetics. The models of its subsystems were built by. C language. The model of the fuel system was attached to the flight simulation and experiment system and ATG test was made. The results show that the model meets the simulation demand.
出处
《机床与液压》
北大核心
2011年第17期104-107,110,共5页
Machine Tool & Hydraulics
基金
国民航局基金资助项目(MHR0703)
