Modeling and software implementation of flight system for simulator of a new fighter  

作　　者：SUICheng-cheng YANGYong-tian JIARong-zhen 

机构地区：[1]SchoolofComputerScienceandTechnology,HarbinEngineeringUniversity,Harbin150001,China [2]BeijingUniversityofAeronauticsandAstronautics,Beijing100083,China

出　　处：《Journal of Marine Science and Application》2004年第1期52-56,共5页船舶与海洋工程学报（英文版）

摘　　要：Real-time modeling and simulation of flight system are the key parts of simulator. After describing the architecture of simulator for a newer fighter, author presents the composition of flight system and its mathematic models. In this paper, aircraft is regarded as an elastic flight body. And a new integrated algorithm which can remedy the shortcoming of Euler method and four-element method is used to calculate the Eulerian angles of aircraft. Finally, the software implementation of the flight system is given in the paper.

关 键 词：flight simulator SIMULATION MODELING six-DOF mathematical model 

分 类 号：V323[航空宇航科学与技术—人机与环境工程]