stability augmentation

The study of the control laws of pitch stability augmentation system with angle-of-attack/ normal acceleration limiter

具有迎角/过载限制器的俯仰增稳系统控制律的研究

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A DSP-Based Joystick in the Stability Augmentation System for Rotary UAV Control Strategy for Tilt-Rotor Aircraft Trimming in Steady Level Flight

基于DSP旋翼飞行机器人增稳操纵杆设计

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The use of H ∞ Control theory has been researched in the design of lateral directional SCAS ( Stability and Control Augmentation System) of armed helicopter. The H ∞ methods are effective in analysis and design of robustness of control system, especially for uncertainties of system.

通过对H∞控制理论在直升机横航向SCAS（增控增稳系统）设计中具体应用的研究，报告了针对不确定的系统，H∞设计方法是进行系统鲁棒性分析和设计的有效方法之一。

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The longitudinal feedback coefficients of a stability augmentation system ( SAS) for a sample aircraft were selected in the light of the condition that the normal acceleration response at the pilot's position approximated to zero.

根据驾驶员位置处法向加速度反应近似为零的条件，选择了算例飞机的纵向增稳器返馈系数。

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On the basis of a250-seat BWB configuration, the control surfaces were first configured according to trim, stability augmentation and maneuverability considerations with margin for disturbances.

本文在一架250座级翼身融合客机布局设计基础上，根据平衡、增稳、机动等要求，设计了操纵面配置方案；

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