This paper presents a novel approach to collision and obstacle avoidance in fixed-wing
unmanned aerial systems (UASs), vehicles with high speed and high inertia, operating in …

Unmanned Aerial Vehicles (UAVs) are increasingly demanded in civil, military and research
purposes. However, they also possess serious threats to the society because faults in UAVs …

This paper presents a novel guidance logic for multi-agent fixed-wing unmanned aerial
systems using a moving mesh method. The moving mesh method is originally designed for …

The main purpose of this paper is to develop an onboard adaptive and robust flight control
system that improves control, stability, and survivability of a small unmanned aerial system in …

This work considers a new” morphing” potential field navigation technique, where potential
fields morph to distribute potential cost to areas necessary for collision avoidance in the …

This paper describes the design of a MIMO H-infinity gain schedule for the Meridian UAS
and illustrates its application for an extended operational range and for a moderate fault …

The focus of this dissertation is the development of control system design algorithms for
autonomous operation of an aircraft in the Martian atmosphere. This research will show …

Undetected failures in critical control systems can be catastrophic, including the loss of
human lives or huge amounts of money. The safety assessment process aims to minimize …

For air-breathing hypersonic cruise vehicles, the flight Mach number control is one of the
important control system task. The velocity of the air-breathing hypersonic cruise vehicle is …

The integral ramjet engine has gained wide popularity as one of the versatile air-breathing
engines for hypersonic flight vehicles. Due to the uniqueness of tightly integrated engine …