This paper presents a framework for the estimated state regulation of the lift force for a
maneuvering wing during a transverse gust encounter. An expression for the effective angle …

This paper presents a framework based on either iterative simulation or iterative
experimentation for constructing an optimal, open-loop maneuver to regulate the …

This work presents an expression for the effective angle of attack of a surging and pitching
wing encountering a transverse gust. Based on this expression, a modified Goman-Khrabrov …

View Video Presentation: https://doi. org/10.2514/6.2021-2937. vid This paper presents a
framework for calculating an optimal pitch maneuver to regulate lift in a transverse gust …

Birds and bats are extraordinarily adept flyers: whether in hunting prey, or evading
predators, their agility and manoeuvrability in flight are characteristics of vital importance …

UNSTEADY aerodynamics is central to research at the interface of fluid dynamics and
control theory for low-Reynolds-number aircraft such as micro air vehicles (MAVs). The …

At high angles of attack or low Reynolds number, aircraft wings or blades of helicopters or
even wind turbines may encounter separation of the ow which can eventually lead to …

This paper describes the implementation of the Goman-Khrabrov model for flow stagnation
near an actuated airfoil with a feedback-controlled pitch rate for the purpose of maximizing …

This research focuses on the improving of dynamic stall control on a wing during rapidly
pitching maneuvers. There are two major components in this research. The rst is modeling …

Modeling of transient blowing actuation using Pulse Width Modulation on a dynamically pitching
NACA 0018 Airfoil Page 1 Modeling of transient blowing actuation using Pulse Width Modulation …