The main task of this work is to design a control system for a small tail-sitter Unmanned
Aerial Vehicle (UAV) during the transition process. Although reasonable control …

In the past few decades, in-flight icing has become a common problem for many missions,
potentially leading to a reduction in control effectiveness and flight stability, which would …

This paper presents a hybrid attitude control scheme of L1 adaptive and dynamic inversion
for unmanned aerial vehicle with actuator faults, where both gain fault and bias fault are …

This paper presents a longitudinal trajectory tracking scheme with L 1 adaptive control for
hypersonic reentry vehicles (HRVs). A linear time-varying (LTV) multiple input multiple …

This paper presents an analysis of the flight parameters and uncertainties that a HiFire 4–
like hypersonic glider experiences through a pull up and a bank maneuver along the …

This paper presents an analysis of the modified L1 adaptive control law. The performance of
this control law is compared to the original control law. The modified L1 control law uses the …

Considering lateral-directional control of an unmanned aerial vehicle (UA V), a multi-input
multi-output (MIMO) control law design method based on L1 adaptive control theory is …

The technology of Bank-to-Turn is an important development direction of hypersonic glide
vehicles' control. But there is a strong coupling between roll channel and yaw channel when …

摘要针对六自由度高超声速飞行器的飞行控制问题, 本文提出了基于非线性动态逆和线性反馈
方法建立主控制系统, 应用L1 自适应控制理论设计辅助控制系统以提升控制性能的设计方案 …