东南大学学报（自然科学版）2012，Vol.42Issue(z1)：186-191,6.DOI:10.3969/j.issn.1001-0505.2012.S1.038
运输机机械操纵系统动力学建模与性能验证
Dynamics modeling and performance verification of the mechanical flight control system on transport airplane
摘要
Abstract
To improve the manipulation performance during the design of the long-span steel cable control system (SCCS) on a large transport airplane (LTA) and obtain an optimal configuration of the mechanical manual flight control system (MMFCS), this paper introduces a new calculation method of equivalent stiffness for the SCCS based on the formula of the equivalent elastic modulus of the steel cables. Then, this paper studies the modeling of the whole MMFCS by multi-degree freedom rigid body dynamics, and the dynamic model of the whole MMFCS is built on a software platform. Thus a new method is provided for the comprehensive performance simulation and the flight quality assessment of the MMFCS. By comparing the digital simulation results with the physical experiment data of the MMFCS, it shows a good reference in engineering design process about the stiffness calculation of long-span SCCS and manipulation performance simulation of the whole MMFCS , and it proves the validity of this proposed method.关键词
大型运输机/机械操纵系统/动力学建模/飞行品质/性能验证Key words
large transport airplane/ mechanical manual flight control system/ dynamics modeling/ flight quality/ performance verification分类
航空航天引用本文复制引用
杨春宁,周国东,李平..运输机机械操纵系统动力学建模与性能验证[J].东南大学学报（自然科学版）,2012,42(z1):186-191,6.基金项目
航空科学基金资助项目(20110776001,飞行器控制一体化技术重点实验室资助)、浙江省自然科学基金资助项目(Y1100696)、中央高校基本科研业务费专项资金资助项目(2011QNA4021,2012QNA4024). （20110776001,飞行器控制一体化技术重点实验室资助）
