导弹驾驶仪稳定回路动态分析系统设计

Design of the dynamic analyse system for missile pilot stabilized loop

为了研究导弹稳定回路的参数对导弹控制系统性能的影响,设计了导弹驾驶仪稳定回路动态分析系统。该系统以工控机为核心,将A/D板,D/A板,定时计数器板按层叠式结构组合在一起,利用了自动化测试设备的硬件设施,并采用了软硬件抗干扰措施,提高了测试分析的精度。测试结果表明该系统能很好的应用于驾驶仪稳定回路测试参数的分析,有很好的理论和应用价值。

For researching parameters of missile stabilized loop to performance effect of missile control system, a dynamic analyse system for missile pilot stabilized loop is devised. The system uses a industrial control computer as a core, the A/D,D/A,and time arithmometer boards are assembled as a cascade structure. Using automatic test hardware facility and increasing software and hardware anti-jamming measures, it improves test precision. Test result indicates that the system can be applied well in the test parameter analyse of the pilot stabilized loop, and has good theory value and practical significance.