摘要
介绍了航空电子综合化仿真系统中任务计算机子系统的设计与实现,详细讨论了此系统的功能、组成以及具体的硬件与软件设计方法。仿真系统的设计采用某型飞机的总线拓扑结构,将各个子系统连接起来,以达到综合显示、综合处理、综合控制、数据综合传输、资源共享的目的,并在综合航电仿真系统的联合调试中,验证了此系统的可行性和正确性。
The design and realization of avionics integrated simulation system about mission computer system was introduced. The functions, composition and the methods of the hardware and software were discussed on emphasis. The system adopted the bus topological structure of a certain aircraft, connecting the various subsystems so as to display, process, control and transmit the data integratedly and share resource. This system could be used in the avionics simulation system for experiment and its feasibility and correctness were validated.
出处
《系统仿真学报》
CAS
CSCD
北大核心
2009年第10期2904-2906,2920,共4页
Journal of System Simulation
基金
航空科学基础基金资助课题(20060553008
05D53021)
关键词
航空电子综合化
任务计算机系统
总线拓扑结构
数字仿真
avionics integrated simulation
mission computer system
bus topological structure
digital simulation