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The Development of the CONDUIT Advanced Control System Design and Evaluation Interface with a Case Study Application to an Advanced Fly by Wire Helicopter DesignThis report details the development and use of CONDUIT (Control Designer's Unified Interface). CONDUIT is a design tool created at Ames Research Center for the purpose of evaluating and optimizing aircraft control systems against handling qualities. Three detailed design problems addressing the RASCAL UH-60A Black Hawk are included in this report to show the application of CONDUIT to helicopter control system design.
Document ID
19990051006
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Colbourne, Jason (California Polytechnic State Univ. San Luis Obispo, CA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1999
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA/TM-1999-208763
A-99V-001
AFDD/TR-99-A-005
NAS 1.15:208763
Report Number: NASA/TM-1999-208763
Report Number: A-99V-001
Report Number: AFDD/TR-99-A-005
Report Number: NAS 1.15:208763
Funding Number(s)
CONTRACT_GRANT: NCC2-983
PROJECT: RTOP 581-30-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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