An IDRA approach for modeling helicopter based on Lagrange dynamics

被引：10
作者：
Li, Yingjie [1 ,2 ]
Zhao, Dingxuan [2 ]
Zhang, Zhongjun [3 ]
Liu, Jingang [3 ]
机构：
[1] Aviat Univ Air Force, Campaign & Command Dept, Changchun 130022, Peoples R China
[2] Jilin Univ, Coll Mech Sci & Engn, Changchun 130022, Peoples R China
[3] Aviat Univ Air Force, Aircraft Dynam Dept, Changchun 130022, Peoples R China
来源：
APPLIED MATHEMATICS AND COMPUTATION | 2015年 / 265卷
基金：
中国国家自然科学基金;
关键词：
IDRA approach; Helicopter; Dynamic model; Real-time; Lagrange equation; CONTROLLER-DESIGN; NONLINEAR CONTROL; IDENTIFICATION; SYSTEM; STABILIZATION; AIRCRAFT; ROBOT;
D O I：
10.1016/j.amc.2015.05.111
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
In order to accelerate the algorithm speed of dynamic model of helicopter, an IDRA approach for modeling helicopter was proposed and a dynamic model of six degrees of freedom (6 DOF) combining flying and landing was established in this paper. As the dynamic model is derived from the Lagrange equation of a non conservative system, treating micro displacements and rotating angles of airframe in a simulation step as generalized coordinates, the relationship between energy dissipation, kinetic energy, potential energy and the generalized coordinates was analyzed. Finally, the reliability of this method and real-time of dynamic model were verified on the experimental platform of helicopter flight simulator, which could provide reliable theoretical foundation for solving the retardance of data transfer of helicopter simulator. (C) 2015 Elsevier Inc. All rights reserved.
引用
收藏
页码：733 / 747
页数：15
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