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Decoupling Control For Oblique-Wing AirplaneTechnical memorandum proposes procedure for mathematical synthesis of control signals proportional to commanded deflections of rudder, elevators, and ailerons of oblique-wing airplane. Procedure designed to generate signals compensating for aerodynamical and inertial cross-coupling among yawing, pitching, and rolling motions. Control interactions decoupled by feedforward and feedback.
Document ID
19920000265
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kempel, Robert W. (NASA Ames Research Center, Moffett Field, CA.)
Pahle, Joseph W. (NASA Ames Research Center, Moffett Field, CA.)
Alag, Gurbux S. (Western Michigan Univ.)
Date Acquired
August 15, 2013
Publication Date
April 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 4
ISSN: 0145-319X
Subject Category
Mathematics And Information Sciences
Report/Patent Number
ARC-11751
Report Number: ARC-11751
ISSN: 0145-319X
Accession Number
92B10265
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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