会议专题

study on change of aircraft center of gravity during fuel consumption

in this paper, the law of change of aircraft center of gravity (CG) during fuel consumption is studied. The change of aircraft CG is discussed based on three different structures, such as single tank system, dual-symmetrical tank system and dual-asymmetrical tank system. Based on dual-symmetrical tank system, two fuel consumption modes are considered including the same consumption rate and different consumption rate on both tanks. The curves of change of aircraft CG on different conditions are obtained. The character and trend of change of CG is analyzed.

fuel consumption change of CG fuel system

Yang Miao Shaoping Wang Yongping Zhao

School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astron School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astron School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astro

国际会议

IEEE 10th International Conference on Industrial Informatics(第十届IEEE工业信息学国际学术会议 INDIN2012)

北京

英文

86-90

2012-07-25(万方平台首次上网日期,不代表论文的发表时间)