摘要
飞行模拟器工程应用中,要求飞机仿真模型按照训练科目要求快速重定位至特定状态,因此快速获得飞机初始状态参数值至关重要。提出一种基于改进Powell算法和飞机飞行动力学模型的配平算法,获取使飞机稳定飞行的状态量和操纵量来实现飞机运动状态参数重定位;根据求解所得运动状态参数和飞机系统仿真原理提出飞机系统状态参数的重定位方法,进而形成飞行模拟器重定位算法架构。将该算法应用于某型号飞行模拟器中进行飞行仿真试验。结果表明:仿真初期飞机平稳飞行,视景画面和运动平台不发生剧烈抖动,提高了仿真训练的逻辑符合性和逼真度,且解算速度较快。
In the application of flight simulator,it is required that the aircraft simulation model quickly relocates to a specific state according to the training subject requirements,so it is crucial to quickly obtain the initial state parameter values of the aircraft.This paper proposes a trimming algorithm based on an improved Powell algorithm and an aircraft flight dynamics model,obtaining state variables and control inputs that enable the aircraft to achieve stable flight,thus realizing the relocation of aircraft motion state parameters.Furthermore,based on the solved motion parameters and aircraft system simulation principles,a repositioning method for aircraft system state parameters is proposed,forming an algorithm architecture for flight simulator repositioning.This algorithm is applied to a specific model of a flight simulator,ensuring stable flight during the initial phase of simulation,with minimal visual and motion platform disturbances,thereby enhancing the logical consistency and realism of the simulation training,and has a faster solving speed.
作者
吴远航
张强
神策
WU Yuanhang;ZHANG Qiang;SHEN Ce(AVIC Aviation Simulation System Co.,Ltd.,Shanghai 201100,China)
出处
《航空工程进展》
2026年第1期149-158,173,共11页
Advances in Aeronautical Science and Engineering
