Transient Analysis of Voltage-Regulated Aircraft D-C Systems
Abstract
The stability of a d-c voltage-regulated aircraft system can be determined by the basic principles of feedback amplifier theory. The transfer function of a shunt-wound d-c generator has been defined and calculated, and a method given for accurately measuring the generator transfer function. There is a calculation of the terminal voltage transient resulting from removal of full load. For this purpose a simplified expression for the transfer function of a carbon pile voltage regulator is presented. The calculated terminal voltage transient is found to be in essential agreement with experiment.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 26, 1949
- Accession Number
- AD1211608
Entities
People
- D. G. Scorgie
Organizations
- United States Naval Research Laboratory