摘要
关于飞机动力学仿真系统设计问题,针对常规气动布局固定翼飞机飞行动力学的特点,给出了具有一般性的飞行动力学计算数学模型,并利用微软ATL组件技术开发了具有跨平台特性的飞行动力学计算组件,在计算功能和应用环境方面具有一定的通用性,可在飞行动力学仿真系统研发时应用,以提高飞行仿真系统研发效率及程序代码的重用性。利用在VC++6.0平台下搭建的MFC—OSG飞行仿真环境对组件进行了应用测试,验证了飞行仿真系统动力学计算模块开发采用组件技术的可行性,具有一定的参考及应用价值。
Aiming at the calculation characteristics of the conventional pneumatic layout of fixed - wing aircraft flight simulation dynamics, through the analysis and induction, the general flight dynamics of the mathematics model was given, and flight dynamics calculation component with the characteristics of cross - platform was developed by u- sing Microsoft ATL component technology. So, the developed component has certain versatility in terms of the calcu- lation function and application environment, so as to achieve the component in the related to flight simulation system research and development of application. Built with the platform of VC ＋ ＋ 6. 0, the MFC - OSG flight simulation visualizing system implemented the application test on the component. The feasibility of using the technology of com- ponent to develop the simulation dynamics module was prove, which has certain reference and application value to some extent.
出处
《计算机仿真》
CSCD
北大核心
2013年第4期49-53,共5页
Computer Simulation
基金
辽宁省自然科学基金计划(2010276)
关键词
动力学模型
飞行仿真
组件
Dynamics model
Flight simulation
Component
