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Dynamic Test and Evaluating System for Flight Control System

机译:飞行控制系统动态测试与评估系统

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This paper presents a prospective study of how to evaluate the overall performance of flight control system based on general purpose computer system. By adopting hardware-in-the-loop simulation (HILS), a simulated real working environment was constructed for flight control system, in which test and evaluation can be accomplished. Because of the strict real-time requirement of HILS, how to implement hard real-time capability in general personal computer systems is analysed systematically. For HILS system, simulation algorithms are different from conventional full digital simulation because of real-time restrictions. And the creditability of simulated work environment is determined not only by computing results, but also by the time when each simulation frame finished. So, Real-time simulation algorithms and the creditability validation of HILS systems are emphasized in the paper as well.
机译:本文介绍了如何评估基于通用计算机系统的飞行控制系统的整体性能的前瞻性研究。通过采用硬件循环仿真(HIL),为飞行控制系统构建了模拟的实际工作环境,其中可以实现测试和评估。由于HIL的严格实时要求,系统系统如何在一般个人计算机系统中实施硬实时能力。对于HILS系统,由于实时限制,仿真算法与传统的全数字模拟不同。并且,模拟工作环境的可信度不仅通过计算结果而确定,而且还确定每个模拟帧完成的时间。因此,本文强调了实时仿真算法和HILS系统的信誉验证。

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