This article presents a command limiting method for attitude protection on aerial vehicles equipped with rate control augmentation systems.The method is developed based on exponential potential functions. To avoid excessive corrections, a switched command limiting control law is proposed. Stability analysis is provided for the closed-loop system. Phase portrait analysis on a linear plant with the proposed method is conducted. Simulation examples of the bank angle protection on a nonlinear transport aircraft model are presented to verify the design.

中文翻译：

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具有速率控制增强系统的飞行器的指令限制

本文提出了一种对装有速率控制增强系统的飞行器进行姿态保护的指令限制方法。该方法是基于指数势函数开发的。为了避免过度修正，提出了一种切换指令限制控制律。为闭环系统提供稳定性分析。使用所提出的方法对线性设备进行相画像分析。介绍了非线性运输机模型上坡度角保护的仿真实例，以验证设计。