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Guidance for a tilt rotor VTOL aircraft during takeoff and landingA perturbation guidance scheme is developed to keep a tilt-rotor VTOL aircraft close to a predetermined nominal flight path during take-off and landing. A simulation of the guidance scheme applied to the Bell Model 266 tilt-rotor VTOL gave satisfactory behavior in the presence of initial errors and wind disturbances.
Document ID
19730015345
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gupta, N. K. (Stanford Univ. CA, United States)
Bryson, A. E., Jr. (Stanford Univ. CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-CR-132043
SUDAAR-448
Report Number: NASA-CR-132043
Report Number: SUDAAR-448
Accession Number
73N24072
Funding Number(s)
CONTRACT_GRANT: NAS2-5143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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