Introduction to Flexible Hypersonic

What is/are Flexible Hypersonic?

Flexible Hypersonic - 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]

flexible hypersonic vehicle

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]

flexible hypersonic flight

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]