Studies of preview gust load alleviation H 2 and H∞ controllers via synthesis, simulation,
wind tunnel tests, and test/simulation correlation are presented in this paper. University of …

The rapid development of aircraft in recent years has attracted more attention, especially the
issue of safe flight for aircraft. Some existing angle detection sensors are difficult to adapt to …

Active gust load alleviation techniques exhibit a high potential in significantly reducing the
transient gust loads on aircraft. In this work the aerodynamic potential of trailing-edge flaps …

View Video Presentation: https://doi. org/10.2514/6.2022-2489. vid This paper describes
simulation and wind tunnel test results of preview gust load alleviation (GLA) controllers …

Preview control using wind estimates derived from Doppler wind lidar measurements is a
promising technique for designing active gust load alleviation functions. Due to the relatively …

Increasing efficiency is at the core of next generation aircraft development. Aerodynamics
can be improved by high aspect ratio wings, but as these wings are more susceptible to …

View Video Presentation: https://doi. org/10.2514/6.2022-0285. vid This work studies the
gust load alleviation of a flexible aircraft equipped with a lidar sensor that measures the wind …

Gust alleviation is of great significance for improving aircraft ride quality and reducing gust
load. Using aircraft response (feedback control) and gust disturbance information …

This paper develops an active disturbance rejection control technology that uses the
equivalent input disturbance (EID) approach to reduce the aeroelastic vibrations and …

In order to reduce the gust response level of the aircraft wing aeroelastic systems in
supersonic flows, the nonlinear energy sink (NES) is introduced into the aeroelastic system …