基于高性能计算机的飞控软件调试系统设计与实现

摘要

An equipment on which airborne missile flight‐control software is debugged and validated ,is designed and implementated against the amount of interface ,the complexity of arithmetic and the real‐time capability .The design and im‐plantation of the equipment is introduced with the key technique .The simulating result on the equipment is given .%空空导弹飞控软件设计中，由于计算机外部接口多、控制算法复杂、实时性要求高，因此调试验证困难，针对其研制了配套设备。该设备以真实的飞控软件作对象，设置匹配接口和必需的外部模型，调试和验证飞控软件。论文介绍了该设备的设计、实现和涉及的关键技术，最后给出了仿真效果。