The design of advanced guidance and control (G&C) systems for space/aerospace vehicles
has received a large amount of attention worldwide during the last few decades and will …

This paper aims to present a new methodology to model the aerodynamic coefficients and
predict the aircraft dynamics under stall conditions, including the hysteresis cycle, using …

This paper presents a new methodology to identify the aerodynamic coefficients and predict
the short-period and phugoid dynamics of an aircraft using two types of supervised learning …

This paper presents the development of direct adaptive control laws to enable an
autonomous unmanned aerial vehicle (UAV) to track reference trajectories in the presence …

Purpose–The purpose of this paper is to analyze and compare the performance of several
different UAV trajectory tracking algorithms in normal and abnormal flight conditions to …

This paper presents a Matlab/Simulink simulation environment developed at West Virginia
University to facilitate the design, testing, and analysis of fault-tolerant control laws for …

Purpose–The purpose of this paper is to gain trajectory-tracking controllers for autonomous
aircraft are optimized using a modified evolutionary, or genetic algorithm (GA) …

This thesis presents the development of a UAV simulation environment for the design,
analysis, and comparison of autonomous flight control laws. The simulation environment …

Biological dendritic cells perform a complex activation/suppression role in the generation,
direction, and control of antibodies. Their action relies on balancing information regarding …

A fault‐tolerant control scheme for the autopilot of the small fixed‐wing UAV is designed and
tested by the actual flight experiments. The small fixed‐wing UAV called Xiang Fei is …