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Control law design to meet constraints using SYNPAC-synthesis package for active controlsMajor features of SYNPAC (Synthesis Package for Active Controls) are described. SYNPAC employs constrained optimization techniques which allow explicit inclusion of design criteria (constraints) in the control law design process. Interrelationships are indicated between this constrained optimization approach, classical and linear quadratic Gaussian design techniques. Results are presented that were obtained by applying SYNPAC to the design of a combined stability augmentation/gust load alleviation control law for the DAST ARW-2.
Document ID
19820014406
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Adams, W. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Tiffany, S. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:83264
NASA-TM-83264
Report Number: NAS 1.15:83264
Report Number: NASA-TM-83264
Meeting Information
Meeting: Joint Automatic Control Conf.
Location: Charlottesville, VA
Country: United States
Start Date: June 17, 1981
End Date: June 19, 1981
Accession Number
82N22280
Funding Number(s)
PROJECT: RTOP 505-34-33-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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