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飞机乘客重量最优布置的一种建模方法

A Model Method of Optimized Passenger Weight Layout
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摘要 飞机重心对飞行安全至关重要,也影响着飞机的性能。本文给出了乘客重量的定义,分析了飞机纵向重心对飞行性能的影响。通过分析确定了以乘客重量为自变量的约束条件和以实现所有乘客的纵向重心坐标靠近重心后极限为目的的目标函数,建立了考察不同重量的乘客在飞机中的座位最优布置的优化模型,并从理论上说明了优化模型具有最优解。算例结果表明,建立的最优化模型存在最优解,用此模型求解目标函数可行。此模型同样适用于行李箱布置与货物装载。 The center of gravity of the aircraft is very important to the flight safety, and it also influences the performance of the aircraft considerably. The definition of the passenger weight is proposed, and the influence of the longitudinal center of gravity on the flight performance is analyzed. Through the analysis, the constrains with passenger weight being independent variables and the objective function that the longitudinal center of gravity of all the passengers is close to the aft center of gravity of the aircraft are built up. To study the optimized passenger layout on the cabin, an optimized model is proposed, and it is explained that this model has an optimized solution in theory. A calculation example is designed, and the result shows that the optimized model has an optimized solution and that to solve the objective function by this model is feasible. In addition, this model is also applicable to the layout of overhead stowage modules and the load of cargo.
作者 王瑞 何政道
出处 《航空科学技术》 2013年第4期43-45,共3页 Aeronautical Science & Technology
关键词 重心 乘客重量 飞行性能 优化模型 center of gravity passenger weight flight performance optimization model
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  • 1.飞机设计的一般技术要求[M].北京:海军司令部,1962..
  • 2.军用飞机飞行品质规范背景材料和使用说明[M].北京:航空工业部,1982..
  • 3.英国空军和海军飞机设计要求(AP970)[M].北京:第三机械工业部六二八研究所,1972..
  • 4.GJBl85—86.有人驾驶飞机(固定翼)飞行品质[S].,..
  • 5肖亚伦,金长江.大气扰动中的飞行原理[M].北京:国防工业出版社,1993.
  • 6Rising J J. Development and flight test evaluation of a pitch stability augmentation system for a relaxed stability 1-1011 [ R]. AIAA S2-1297,1982.
  • 7Ward Greta N, Ly Uy-Loi. Stability augmentation design of a large subsonic transport [ R ]. AIAA 94-3590- CP,1994.
  • 8Blight J D, Gangsaas D, Richardson T M. Control law synthesis for an airplane with relaxed static stability [ J ]. AIAA Journal of Guidance, Control,and Dynamics, 1986, 9(5 ) :546-554.
  • 9Sobel K M. Model reference adaptive control for a relaxed static stability aircraft [ C]//21st IEEE Conference on Decision and Control. 1984 : 1369-1373.
  • 10Doyle J C, Stein G. Multivariable feedback design concepts for a classical/modem synthesis [ J ]. IEEE Transactions on Automatic Control, 1981, AC-26 ( 1 ) :4-16.

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