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High-Alpha Research Vehicle (HARV) longitudinal controller: Design, analyses, and simulation resultssThis paper describes the design, analysis, and nonlinear simulation results (batch and piloted) for a longitudinal controller which is scheduled to be flight-tested on the High-Alpha Research Vehicle (HARV). The HARV is an F-18 airplane modified for and equipped with multi-axis thrust vectoring. The paper includes a description of the facilities, a detailed review of the feedback controller design, linear analysis results of the feedback controller, a description of the feed-forward controller design, nonlinear batch simulation results, and piloted simulation results. Batch simulation results include maximum pitch stick agility responses, angle of attack alpha captures, and alpha regulation for full lateral stick rolls at several alpha's. Piloted simulation results include task descriptions for several types of maneuvers, task guidelines, the corresponding Cooper-Harper ratings from three test pilots, and some pilot comments. The ratings show that desirable criteria are achieved for almost all of the piloted simulation tasks.
Document ID
19950004448
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ostroff, Aaron J.
(NASA Langley Research Center Hampton, VA, United States)
Hoffler, Keith D.
(NASA Langley Research Center Hampton, VA, United States)
Proffitt, Melissa S.
(NASA Langley Research Center Hampton, VA, United States)
Brown, Philip W.
(NASA Langley Research Center Hampton, VA, United States)
Phillips, Michael R.
(NASA Langley Research Center Hampton, VA, United States)
Rivers, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Messina, Michael D.
(NASA Langley Research Center Hampton, VA, United States)
Carzoo, Susan W.
(NASA Langley Research Center Hampton, VA, United States)
Bacon, Barton J.
(NASA Langley Research Center Hampton, VA, United States)
Foster, John F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-17323
NAS 1.60:3446
NASA-TP-3446
Report Number: L-17323
Report Number: NAS 1.60:3446
Report Number: NASA-TP-3446
Accession Number
95N10860
Funding Number(s)
PROJECT: RTOP 505-68-30-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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