基于LQR/LQG控制策略的通用航空数字自动驾驶仪设计

2017 IEEE/AIAA 36th Digital Avionics Systems Conference (DASC) Pub Date : 2017-09-01 DOI:10.1109/DASC.2017.8102058

J. Vlk, Peter Chudý

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引用次数: 6

摘要

本文介绍了线性二次型调节器(LQR) /线性二次型高斯控制器(LQG)的设计及相关的基本理论。数字自动驾驶仪的LQR/LQG控制器进行了性能评估测试，该测试考虑了监管机构发布的各种性能和稳定性要求。在通用航空飞机仿真模型上验证了该设计的鲁棒性。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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General aviation digital autopilot design based on LQR/LQG control strategy

The paper introduces a description of a Linear Quadratic Regulator (LQR) / Linear Quadratic Gaussian (LQG) controller design along with related basic theory. The LQR/LQG controller of a digital autopilot is subjected to performance evaluation tests, which consider various performance and stability requirements issued by the regulatory agencies. The design's robustness is tested on a General Aviation aircraft simulation model.

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2017 IEEE/AIAA 36th Digital Avionics Systems Conference (DASC)

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