Adaptive control of aircraft in windshear

Adaptive control of aircraft in windshear
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风切变中飞机的自适应控制

DOI：
10.1109/cdc.1991.261518
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发表时间：
1991
期刊：
[1991] Proceedings of the 30th IEEE Conference on Decision and Control
影响因子：
--
通讯作者：
E. Ryan
E. Ryan
中科院分区：
--
文献类型：
--
作者：
G. Leitmann;S. Pandey;E. Ryan

文献摘要

被引文献

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起飞后遇到风切变的飞机的控制被视为将爬升率稳定在期望值附近的问题。开发了一种仅使用爬升率信息的自适应策略。通过采用四种不同的风切变模型的模拟来说明相对于风切变结构和强度的鲁棒性。对配备三台 JT8D-17 涡轮风扇发动机的波音 727 飞机进行了模拟。<<ETX>>
The control of an aircraft encountering windshear after takeoff is treated as a problem of stabilizing the climb rate about a desired value. An adaptive strategy is developed which uses only climb rate information. Robustness vis-a-vis windshear structure and intensity is illustrated via simulations employing four different windshear models. Simulations were carried out for a Boeing-727 aircraft with three JT8D-17 turbofan engines.<<ETX>>