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Generalized Predictive Control of Dynamic Systems with Rigid-Body ModesNumerical simulations to assess the effectiveness of Generalized Predictive Control (GPC) for active control of dynamic systems having rigid-body modes are presented. GPC is a linear, time-invariant, multi-input/multi-output predictive control method that uses an ARX model to characterize the system and to design the controller. Although the method can accommodate both embedded (implicit) and explicit feedforward paths for incorporation of disturbance effects, only the case of embedded feedforward in which the disturbances are assumed to be unknown is considered here. Results from numerical simulations using mathematical models of both a free-free three-degree-of-freedom mass-spring-dashpot system and the XV-15 tiltrotor research aircraft are presented. In regulation mode operation, which calls for zero system response in the presence of disturbances, the simulations showed reductions of nearly 100%. In tracking mode operations, where the system is commanded to follow a specified path, the GPC controllers produced the desired responses, even in the presence of disturbances.
Document ID
20130011697
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Kvaternik, Raymond G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
April 1, 2013
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA/TM-2013-217976
NF1676L-15781
L-20211
Report Number: NASA/TM-2013-217976
Report Number: NF1676L-15781
Report Number: L-20211
Funding Number(s)
WBS: WBS 432938.11.01.07.43.40.08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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