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Characterization of a Recoverable Flight Control Computer System

机译:可恢复飞行控制计算机系统的特性

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摘要

The design and development of a Closed-Loop System to study and evaluate the performance of the Honeywell Recoverable Computer System (RCS) in electromagnetic environments (EME) is presented. The development of a Windows-based software package to handle the time-critical communication of data and commands between the RCS and flight simulation code in real-time while meeting the stringent hard deadlines is also submitted. The performance results of the RCS and characteristics of its upset recovery scheme while exercising flight control laws under ideal conditions as well as in the presence of electromagnetic fields are also discussed.
机译:介绍了一种用于研究和评估霍尼韦尔可恢复计算机系统(RCS)在电磁环境(EME)中的性能的闭环系统的设计和开发。还提交了基于Windows的软件包的开发,以在严格的严格期限内实时处理RCS与飞行模拟代码之间的时间紧迫的数据和命令通信。还讨论了RCS的性能结果及其不正常恢复方案的特征,同时在理想条件下以及在存在电磁场的情况下行使飞行控制律。

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