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The C-5A active lift distribution control systemThe ALDCS development and design tasks, ALDCS functional configuration, and resulting challenges encountered while accomplishing the first phase of the program are described. These tasks are establishing system requirements and criteria and synthesizing a system mechanization to meet the desired load alleviation, stability margins, flight safety, and flying qualities performance. Results of the ALDCS development and prototype system flight simulation programs, and control law optimization including system stability, handling qualities and structural load analyses are presented, along with concluding remarks relative to the system design integration.
Document ID
19760024060
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hargrove, W. J.
(Lockheed Aircraft Corp. Marietta, GA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Stability And Control
Accession Number
76N31148
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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