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A simulation study of the flight dynamics of elastic aircraft. Volume 1: Experiment, results and analysisThe simulation experiment described addresses the effects of structural flexibility on the dynamic characteristics of a generic family of aircraft. The simulation was performed using the NASA Langley VMS simulation facility. The vehicle models were obtained as part of this research. The simulation results include complete response data and subjective pilot ratings and comments and so allow a variety of analyses. The subjective ratings and analysis of the time histories indicate that increased flexibility can lead to increased tracking errors, degraded handling qualities, and changes in the frequency content of the pilot inputs. These results, furthermore, are significantly affected by the visual cues available to the pilot.
Document ID
19880004717
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Waszak, Martin R.
(Purdue Univ. West Lafayette, IN, United States)
Davidson, John B.
(Purdue Univ. West Lafayette, IN, United States)
Schmidt, David K.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1987
Publication Information
Publisher: NASA
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-4102
NAS 1.26:4102
Report Number: NASA-CR-4102
Report Number: NAS 1.26:4102
Accession Number
88N14099
Funding Number(s)
PROJECT: RTOP 505-66-01-02
CONTRACT_GRANT: NAG1-254
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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