The objective of this chapter is to develop a unified actuator nonlinearity compensation scheme for an aircraft augmented with SJs operating at a wide range of conditions, including both low and high AoA. The motivation for such a design is the intrinsically complicated nonlinear characteristic of a SJ when used for an aircraft operating in a wide range of AoA.
Adaptive Synthetic Jet Actuation for Aircraft Control
Studies in Systems, Decision and Control
Adaptive Compensation of Nonlinear Actuators for Flight Control Applications ; Kapitel : 7 ; 113-129
23.07.2021
17 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch