基于分岔控制的大迎角飞行动力学非线性镇定

1990 American Control Conference Pub Date : 1990-05-23 DOI:10.23919/ACC.1990.4791129

E. Abed, Hsien-Chiarn Lee

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引用次数: 21

摘要

我们考虑了在大迎角范围内飞行的稳定控制律的设计问题，该控制律同时也用于向飞行员发出即将失速的信号。本文将分岔镇定与传统的线性控制系统设计相结合。为了集中讨论，对F-8“十字军”战斗机的纵向动力学模型进行了详细的分析。

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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Nonlinear Stabilization of High Angle-of-Attack Flight Dynamics using Bifurcation Control

We consider the problem of designing stabilizing control laws for flight over a broad range of angles-of-attack which also serve to signal the pilot of impending stall. The paper employs bifurcation stabilization coupled with more traditional linear control system design. To focus the discussion, a detailed analysis is given for a model of the longitudinal dynamics of an F-8 Crusader.

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来源期刊

1990 American Control Conference

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