6533b856fe1ef96bd12b1d8a

RESEARCH PRODUCT

Hidden attractors in aircraft control systems with saturated inputs

B. R. AndrievskyE. V. KudryashovaN. V. KuznetsovO. A. KuznetsovaG. A. Leonov

subject

FOS: Electrical engineering electronic engineering information engineeringFOS: MathematicsComputer Science - Systems and ControlSystems and Control (eess.SY)Dynamical Systems (math.DS)Mathematics - Dynamical Systems

description

In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft pilot involved oscillations (PIO) phenomenon and the airfoil flutter suppression system.

https://dx.doi.org/10.48550/arxiv.1711.10302