A morphing missile aims to get optimal flight performances at different flight conditions by a
variable aerodynamic shape according to the requirements of multiple missions. For a long …

The modeling and tracking control of variable-wingspan aircraft are researched based on TS
fuzzy theory. The relationship between aerodynamic parameters and variation rate of aircraft …

无人机(Unmanned aerial vehicle, UAV) 的栖落机动是一种大幅度的俯仰运动,
易引起升降舵操纵力矩饱和. 本文以变体方式增强无人机的俯仰操纵能力, 并研究其对应的控制 …

The problem of cooperative control of morphing aircraft during deformable flight is studied.
The object is a morphing aircraft with retractable wings. Firstly, the characteristics of …

In this paper, we address the problem of altitude and velocity controllers design for variable-
sweep aircraft with model uncertainties. The object is to maintain altitude and velocity during …