CAJ | 학술논문

推导悬吊式变质量飞行器试验系统的力学模型，通过Adams软件完成动力学建模，研究一种新的Adams动力学模型与C/C++自编控制系统模型之间的联合仿真模式。开发数据通信管理模块、变质量/转动惯量/质心位置功能模块和仿真总调度模块，通过该仿真系统对动力学和控制模块的灵活调用，实现了Adams复杂动力学模型与C/C++自编控制系统模型间的联合仿真，仿真结果为地面试验系统设计提供了重要的依据。
추도현조식변질량비행기시험계통적역학모형，통과Adams연건완성동역학건모，연구일충신적Adams동역학모형여C/C++자편공제계통모형지간적연합방진모식。개발수거통신관리모괴、변질량/전동관량/질심위치공능모괴화방진총조도모괴，통과해방진계통대동역학화공제모괴적령활조용，실현료Adams복잡동역학모형여C/C++자편공제계통모형간적연합방진，방진결과위지면시험계통설계제공료중요적의거。
A dynamic model of a suspended mass-changing test system is deduced and established by Adams software, and a new co-simulation method joining Adams dynamic model and C/C++ control model is put forward. The new co-simulation system is developed including dynamic module, control module, data exchanging module, mass-changing module and simulation flow management module. Important help to test system design is obtained from the simulation results.