The work presented in this research focuses on the design of a robust nonlinear flight control
system for a small fixed-wing UAV against uncertainties and external disturbances. Toward …

This paper focuses on the design of a disturbance rejection controller for a tailless aircraft
based on the technique of nonlinear dynamic inversion (NDI). The tailless aircraft model …

View Video Presentation: https://doi. org/10.2514/6.2022-2049. vid The high-altitude aerial
platform concept called “Mothership” is a tethered wing that flies at altitudes higher than …

The flight dynamics of small Unmanned Aerial Vehicles (UAVs) exhibits substantial
nonlinear features which should not be ignored in simulation or analysis. In this work, a …

Robust control has been successful in enabling flight stability and performance for UAVs.
This paper presents a simple explainable robust control design for UAV platforms with non …

建立了无人机飞行动力学模型, 设计了PD 控制算法对无人机进行轨迹跟踪控制; 基于Isight
软件将多岛遗传算法和序列二次规划法相结合, 对PD 控制系数进行了优化调节 …

Awareness in guidance and control system design has increased strongly due to the
enormous developments in Unmanned Aerial vehicles (UAVs) as well as their wide …

Unmanned vehicles of all categories, including air, sea, land, and space, have become the
current trend in the military and civilian fields of many countries [1]. As a result, autonomous …

This work presents four control laws applied to path following with a fixed-wing unmanned
aerial vehicle, and such control laws are compared to know which of them achieved the …

The Thrust vector control (TVC) is a method for controlling the angular velocity and attitude
of aerial vehicles (AV) by manipulating the thrust direction of propulsion. This technology …