Automatic landing of aircraft is a challenging guidance and control task that requires multiple
feedback loops and a precise sequence of actions. Increasing operational flexibility and …

The model-based flight control system design for a highly flexible flutter demonstrator,
developed in the European FLEXOP project, is presented. The flight control system includes …

This paper demonstrates the utility of novel probabilistic robustness analysis tools on an
industry-sized autolanding system of a civil transport aircraft. The closed-loop aircraft model …

A low-complexity anti-windup compensation scheme for linear parameter-varying (LPV)
controllers is proposed in this paper. Anti-windup compensation usually increases …

This paper presents a systematic linear parameter varying (LPV) control approach for the 3-
axis attitude control of an Earth-observation satellite in a sun-synchronous orbit. The …

A comprehensive design of the baseline control and navigation system for a single-jet-
engined flutter demonstrator aircraft is presented in this paper. To facilitate the design task, a …

The landing phase during a flight probably is the most dangerous part, as most of the
accidents occur in this phase. A robust trajectory tracking controller is presented to autoland …

Quick and high-fidelity updates about aerodynamic loads of large-scale structures, from
trains, planes, and automobiles to many civil infrastructures, serving under the influence of a …

A complete flight control architecture with two different operating modes is developed for a
24.6 kg UAV. The first control mode provides easy-handling of the UAV for a remote pilot …

Abstract We describe the Intelligent Autopilot System (IAS), a fully autonomous autopilot
capable of piloting large jets such as airliners by learning from experienced human pilots …