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
Analysis of a control system containing two nonlinearitiesParameter plane method of stability analysis applied to spacecraft attitude control system with two nonlinearities related by nonlinear differential equation
Document ID
19700056916
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Seltzer, S. M.
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publisher: WESTERN PERIODICALS CO.,
Subject Category
Electronics
Meeting Information
Meeting: ASILOMAR CONFERENCE ON CIRCUITS AND SYSTEMS, 3RD
Location: PACIFIC GROVE, CA
Start Date: December 10, 1969
End Date: December 12, 1969
Sponsors: ASILOMAR CONFERENCE ON CIRCUITS AND SYSTEMS
Accession Number
70A33032
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

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