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A Control Law Design Method Facilitating Control Power, Robustness, Agility, and Flying Qualities Tradeoffs: CRAFTA multi-input, multi-output control law design methodology, named "CRAFT", is presented. CRAFT stands for the design objectives addressed, namely, Control power, Robustness, Agility, and Flying Qualities Tradeoffs. The methodology makes use of control law design metrics from each of the four design objective areas. It combines eigenspace assignment, which allows for direct specification of eigenvalues and eigenvectors, with a graphical approach for representing the metrics that captures numerous design goals in one composite illustration. Sensitivity of the metrics to eigenspace choice is clearly displayed, enabling the designer to assess the cost of design tradeoffs. This approach enhances the designer's ability to make informed design tradeoffs and to reach effective final designs. An example of the CRAFT methodology applied to an advanced experimental fighter and discussion of associated design issues are provided.
Document ID
19990025985
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Murphy, Patrick C.
(NASA Langley Research Center Hampton, VA United States)
Davidson, John B.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1998
Subject Category
Aircraft Stability And Control
Report/Patent Number
L-17571
NASA/TP-1998-208463
NAS 1.60:208463
Report Number: L-17571
Report Number: NASA/TP-1998-208463
Report Number: NAS 1.60:208463
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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