NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
ASDTIC - A feedback control innovation.The ASDTIC (analog signal to discrete time interval converter) control subsystem provides precise output control of high performance aerospace power supplies. The key to ASDTIC operation is that it stably controls output by sensing output energy change as well as output magnitude. The ASDTIC control subsystem and control module were developed to improve power supply performance during static and dynamic input voltage and output load variations, to reduce output voltage or current regulation due to component variations or aging, to maintain a stable feedback control with variations in the loop gain or loop time constants, and to standardize the feedback control subsystem for power conditioning equipment.
Document ID
19730030099
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lalli, V. R.
(NASA Lewis Research Center Spacecraft Technology Div., Cleveland, Ohio, United States)
Schoenfeld, A. D.
(NASA Lewis Research Center Cleveland, Ohio; TRW Systems Group, Redondo Beach, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 72-1057
Meeting Information
Meeting: Joint Propulsion Specialist Conference
Location: New Orleans, LA
Country: US
Start Date: November 29, 1972
End Date: December 1, 1972
Sponsors: American Institute of Aeronautics and Astronautics, Society of Automotive Engineers
Accession Number
73A14901
Funding Number(s)
CONTRACT_GRANT: NAS12-2017
CONTRACT_GRANT: NAS3-14392
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available