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NASA NTRS · 20040085796

LPV Antiwindup Compensation for Enhanced Flight Control Performance

Abstract

In this paper, we propose a saturation control scheme for linear parameter-varying (LPV) systems from an antiwindup control perspective. The proposed control approach is advantageous because it can be thought of as an augmented control algorithm from the existing control system. Moreover, the synthesis condition for an antiwindup compensator is formulated as a linear matrix inequality (LMI) optimization problem and can be solved efficiently. We have applied the LPV antiwindup controller to an F-16 longitudinal autopilot control system design to enhance aircraft safety and improve flight quality in a high angle of attack region.

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BibTeXRIS

Lu, Bei, Wu, Fen, Kim, Sung-Wan. 2003-01-01. LPV Antiwindup Compensation for Enhanced Flight Control Performance. https://ntrs.nasa.gov/citations/20040085796

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