LPV Antiwindup Compensation for Enhanced Flight Control PerformanceIn 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.
Document ID
20040085796
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Lu, Bei (North Carolina State Univ. Raleigh, NC, United States)
Wu, Fen (North Carolina State Univ. Raleigh, NC, United States)
Kim, Sung-Wan (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 2003-5495Report Number: AIAA Paper 2003-5495
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Austin, TX
Country: United States
Start Date: August 11, 2003
End Date: August 14, 2003
Sponsors: American Inst. of Aeronautics and Astronautics