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Design and evaluation of a Stochastic Optimal Feed-forward and Feedback Technology (SOFFT) flight control architectureThis paper describes the design and evaluation of a stochastic optimal feed-forward and feedback technology (SOFFT) control architecture with emphasis on the feed-forward controller design. The SOFFT approach allows the designer to independently design the feed-forward and feedback controllers to meet separate objectives and then integrate the two controllers. The feed-forward controller has been integrated with an existing high-angle-of-attack (high-alpha) feedback controller. The feed-forward controller includes a variable command model with parameters selected to satisfy level 1 flying qualities with a high-alpha adjustment to achieve desired agility guidelines, a nonlinear interpolation approach that scales entire matrices for approximation of the plant model, and equations for calculating feed-forward gains developed for perfect plant-model tracking. The SOFFT design was applied to a nonlinear batch simulation model of an F/A-18 aircraft modified for thrust vectoring. Simulation results show that agility guidelines are met and that the SOFFT controller filters undesired pilot-induced frequencies more effectively during a tracking task than a flight controller that has the same feedback control law but does not have the SOFFT feed-forward control.
Document ID
19940032506
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ostroff, Aaron J.
(NASA Langley Research Center Hampton, VA, United States)
Proffitt, Melissa S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TP-3419
L-17273
NAS 1.60:3419
Report Number: NASA-TP-3419
Report Number: L-17273
Report Number: NAS 1.60:3419
Accession Number
94N37014
Funding Number(s)
PROJECT: RTOP 505-64-30-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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