The unknown disturbances and the changing uncertainties bring difficulties for designing a
stable attitude controller for UAV. In this paper, a novel adaptive fault‐tolerant attitude control …

The wing‐in‐ground effect craft (WIG craft) is a kind of vehicle that flies close to the ground to
achieve a flight with low aerodynamic drag and high lift. A robust and precise height control …

Unmanned Aero Vehicles (UAV) has become a useful entity for quite a good number of
industries and facilities. It is an agile, cost effective and reliable solution for communication …

Rejection of external disturbances is vital for small aircraft flying in environments with
dynamic flow fields, especially due to their increased sensitivity to disturbances. Fixed wing …

The UAV (Unmanned Aerial Vehicles) they have demonstrated their enormous capabilities
in military and civilian applications in recent years. They have become an indispensable tool …

In this paper we build an ODSMC (Output Feedback Discrete Time Sliding Mode Control)
controller for a fixed-winged aircraft. ODSMC control is employed, which is widely utilized in …

This paper aims at exploring a new-type mode for autolanding control of fixed-wing
unmanned aerial vehicles (UAVs). A discrete-time data-driven control scheme is tentatively …

The reason why the measurement precision of the aeromagnetic data cannot be as high as
that of the aeromagnetic instruments is due to the level of magnetic interference of an …

Unmanned Aerial Vehicles (UAVs) are used for wide range of applications in both military
and civil operations. Flight control systems (FCS) and simulators are used for the control and …

This work focuses on flight controller design and aircraft geometric parameter optimization
without explicitly using the aircraft mathematical model and its transfer functions. The design …