NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Additional studies of quasi-optimum feedback control techniquesQuasi-optimal control technique for space vehicle attitude, bounded acceleration rendezvous in free space, and aircraft landing problem
Document ID
19680018835
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Friedland, B. (General Precision, Inc. Little Falls, NJ, United States)
Ling, C. K. (General Precision, Inc. Little Falls, NJ, United States)
Schilder, M. (General Precision, Inc. Little Falls, NJ, United States)
Thau, F. E. (General Precision, Inc. Little Falls, NJ, United States)
Welt, S. (General Precision, Inc. Little Falls, NJ, United States)
Date Acquired
August 4, 2013
Publication Date
July 1, 1968
Publication Information
Publisher: NASA
Subject Category
Electronics
Report/Patent Number
NASA-CR-1099
Report Number: NASA-CR-1099
Accession Number
68N28307
Funding Number(s)
CONTRACT_GRANT: NAS2-3636
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available