Improvements in reliability, safety, and operational efficiency of aeroengines can be brought
in a cost‐effective way using advanced control concepts, thus requiring only software …

Offshore wind energy is expected to provide a significant contribution to the achievement of
the European Renewable Energy targets. One of the main technological issues affecting …

In this paper, an incremental nonlinear dynamic inversion (INDI) control scheme is proposed
for the attitude tracking of a helicopter with model uncertainties, and actuator delay and …

Helicopters are highly nonlinear and internally unstable air vehicles, the dynamic response
of which can be strongly influenced by flight conditions (wind gust, ground effect, etc.) …

Low-altitude flight in mountainous terrains is a difficult flight task applied in both military and
civilian fields. The helicopter has to maintain low altitude to realize search and rescue …

This paper treats a robust adaptive trajectory-tracking control design for a rotorcraft using a
high-fidelity math model subject to model uncertainties. In order to control the nonlinear …

Controller design for airplane flight control is challenged to achieve an optimum result,
particularly for safety purposes. The experiment evaluated the linear quadratic regulator …

Quad‐Tilt‐Wing (QTW) Unmanned Aerial Vehicle (UAV) is one of the promising types of
UAVs because of its high‐speed cruise performance similar to fixed‐wing aircraft and VTOL …

A novel continuous sliding mode control (CSMC) strategy based on the finite‐time
disturbance observer (FTDO) is proposed for the small‐scale unmanned helicopters in the …

This study addresses the design of a full-authority Attitude Command-Attitude Hold flight
control system for the Bo-105 helicopter. A single sixth-order dynamic controller replaces the …