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Adaptive Data-based Predictive Control for Short Take-off and Landing (STOL) AircraftData-based Predictive Control is an emerging control method that stems from Model Predictive Control (MPC). MPC computes current control action based on a prediction of the system output a number of time steps into the future and is generally derived from a known model of the system. Data-based predictive control has the advantage of deriving predictive models and controller gains from input-output data. Thus, a controller can be designed from the outputs of complex simulation code or a physical system where no explicit model exists. If the output data happens to be corrupted by periodic disturbances, the designed controller will also have the built-in ability to reject these disturbances without the need to know them. When data-based predictive control is implemented online, it becomes a version of adaptive control. The characteristics of adaptive data-based predictive control are particularly appropriate for the control of nonlinear and time-varying systems, such as Short Take-off and Landing (STOL) aircraft. STOL is a capability of interest to NASA because conceptual Cruise Efficient Short Take-off and Landing (CESTOL) transport aircraft offer the ability to reduce congestion in the terminal area by utilizing existing shorter runways at airports, as well as to lower community noise by flying steep approach and climb-out patterns that reduce the noise footprint of the aircraft. In this study, adaptive data-based predictive control is implemented as an integrated flight-propulsion controller for the outer-loop control of a CESTOL-type aircraft. Results show that the controller successfully tracks velocity while attempting to maintain a constant flight path angle, using longitudinal command, thrust and flap setting as the control inputs.
Document ID
20100022785
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Barlow, Jonathan Spencer
(Stinger Ghaffarin Technologies, Inc. Greenbelt, MD, United States)
Acosta, Diana Michelle
(NASA Ames Research Center Moffett Field, CA, United States)
Phan, Minh Q.
(Dartmouth Coll. Hanover, NH, United States)
Date Acquired
August 24, 2013
Publication Date
April 6, 2010
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN522
Report Number: ARC-E-DAA-TN522
Meeting Information
Meeting: AIAA Infotech@Aerospace
Location: Seattle, WA
Country: United States
Start Date: April 6, 2009
End Date: April 9, 2009
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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