Flexible Hypersonic(灵活的高超声速)研究综述
Flexible Hypersonic 灵活的高超声速 - In this article, an integrated guidance and control design method for general nonlinear flexible hypersonic flight vehicles in the presence of dynamic uncertainties based on the L 1 adaptive state feedback control approach is presented. [1] This study develops a novel neural-approximation-based prescribed performance controller for flexible hypersonic flight vehicles (HFVs). [2] This paper addresses a fault accommodation issue for flexible hypersonic vehicles by the static output feedback. [3] A velocity L1 adaptive controller and an altitude L1 adaptive controller are designed to control flexible hypersonic vehicle model with actuator loss fault. [4] In this article, we examine the system control design of a flexible hypersonic vehicle with an unknown direction control. [5] In this paper, the reference tracking problem for a class of flexible hypersonic vehicles, whose dynamics vary significantly as flight states changes, is investigated via a novel switched linear parameter-varying (LPV) framework. [6] Considering the nonlinearity, uncertainty, and rigid/elastic coupling, a state/parameter joint estimation method is essential for control system design or fault diagnosis of flexible hypersonic vehicles. [7] The design is applied to the flexible hypersonic flight dynamics and a better tracking performance is obtained. [8]本文提出了一种基于L 1 自适应状态反馈控制方法的一般非线性柔性高超声速飞行器存在动态不确定性的综合制导与控制设计方法。 [1] 本研究为灵活的高超音速飞行器 (HFV) 开发了一种新的基于神经逼近的规定性能控制器。 [2] 本文通过静态输出反馈解决了柔性高超声速飞行器的故障适应问题。 [3] 设计了速度L1自适应控制器和高度L1自适应控制器来控制具有执行器丢失故障的柔性高超声速车辆模型。 [4] 在本文中,我们研究了具有未知方向控制的柔性高超声速飞行器的系统控制设计。 [5] 在本文中,通过一种新颖的切换线性参数变化(LPV)框架研究了一类柔性高超音速飞行器的参考跟踪问题,其动力学随着飞行状态的变化而显着变化。 [6] 考虑到非线性、不确定性和刚/弹性耦合,状态/参数联合估计方法对于柔性高超声速飞行器的控制系统设计或故障诊断至关重要。 [7] 将该设计应用于柔性高超声速飞行动力学,获得了较好的跟踪性能。 [8]
flexible hypersonic vehicle 柔性高超声速飞行器
This paper addresses a fault accommodation issue for flexible hypersonic vehicles by the static output feedback. [1] A velocity L1 adaptive controller and an altitude L1 adaptive controller are designed to control flexible hypersonic vehicle model with actuator loss fault. [2] In this article, we examine the system control design of a flexible hypersonic vehicle with an unknown direction control. [3] In this paper, the reference tracking problem for a class of flexible hypersonic vehicles, whose dynamics vary significantly as flight states changes, is investigated via a novel switched linear parameter-varying (LPV) framework. [4] Considering the nonlinearity, uncertainty, and rigid/elastic coupling, a state/parameter joint estimation method is essential for control system design or fault diagnosis of flexible hypersonic vehicles. [5]本文通过静态输出反馈解决了柔性高超声速飞行器的故障适应问题。 [1] 设计了速度L1自适应控制器和高度L1自适应控制器来控制具有执行器丢失故障的柔性高超声速车辆模型。 [2] 在本文中,我们研究了具有未知方向控制的柔性高超声速飞行器的系统控制设计。 [3] 在本文中,通过一种新颖的切换线性参数变化(LPV)框架研究了一类柔性高超音速飞行器的参考跟踪问题,其动力学随着飞行状态的变化而显着变化。 [4] 考虑到非线性、不确定性和刚/弹性耦合,状态/参数联合估计方法对于柔性高超声速飞行器的控制系统设计或故障诊断至关重要。 [5]
flexible hypersonic flight 灵活的高超声速飞行
In this article, an integrated guidance and control design method for general nonlinear flexible hypersonic flight vehicles in the presence of dynamic uncertainties based on the L 1 adaptive state feedback control approach is presented. [1] This study develops a novel neural-approximation-based prescribed performance controller for flexible hypersonic flight vehicles (HFVs). [2] The design is applied to the flexible hypersonic flight dynamics and a better tracking performance is obtained. [3]本文提出了一种基于L 1 自适应状态反馈控制方法的一般非线性柔性高超声速飞行器存在动态不确定性的综合制导与控制设计方法。 [1] 本研究为灵活的高超音速飞行器 (HFV) 开发了一种新的基于神经逼近的规定性能控制器。 [2] 将该设计应用于柔性高超声速飞行动力学,获得了较好的跟踪性能。 [3]