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Development of methods for the analysis and evaluation of CCV aircraftThe development of an advanced, computerized method for the analysis and evaluation of the aeroelastic stability and control parameters of controls fixed and controls free flight vehicles is presented. Specifically, the Level 2.01 FLEXSTAB computer program system is described. Technical areas in aerodynamics, dynamics, and control system synthesis are defined in which further research and development are planned to extend the analysis capability of the system for future CCV applications.
Document ID
19760024083
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schwanz, R. C. (Air Force Flight Dynamics Lab. Wright-Patterson AFB, OH, 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 Design, Testing And Performance
Accession Number
76N31171
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760024047Collected WorksAdvanced Control Technology and its Potential for Future Transport Aircraft
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