Gust Alleviation Device Applied to the Sensorcraft Structure

摘要

A gust alleviation model is presented and its effectiveness will be demonstrated on the sensorcraft structure. A simple rectangular wing will be used to perform a parametric study in order to study the effect of the different parameters, such as stiffness attachment, sweep, size of gust device, etc. Consideration is made of the feasibility of incorporating an adaptive torsional stiffness attachment that could be used to trim the device for more efficient flight, and also to enable roll control.