Power System Control Study. Phase I - Integrated Control Techniques

This report documents the Phase I results of a two phase study program which addresses the integration of advanced power system control technologies into a reliable and fault tolerant system. The advanced control technologies integrated include electric engine start, automatic load management, micro...

Full description

Saved in:
Bibliographic Details
Main Authors: Lautner ,D E, Marek ,A J, Perkins,J R
Format: Report
Language:English
Subjects:
Aircraft
AIRCRAFT EQUIPMENT
BUS CONDUCTORS
CONTROL SYSTEMS
Cycloconverters
ELECTRIC GENERATORS
ELECTRIC MOTORS
ELECTRIC POWER DISTRIBUTION
Electric Power Production and Distribution
ELECTRICAL EQUIPMENT
EMUX(Electrical Multiplexing)
ENGINE STARTERS
IDG(Integrate Drive Generators)
INTEGRATED SYSTEMS
MICROPROCESSORS
MULTIPLEXING
PE62203F
VSCF(Variable Speed Constant Frequency)
WUAFAPL31452954
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:This report documents the Phase I results of a two phase study program which addresses the integration of advanced power system control technologies into a reliable and fault tolerant system. The advanced control technologies integrated include electric engine start, automatic load management, microprocessor control implementations, design techniques for providing 'no-gap' power and an all 'solid state' electric power distribution system. Electric system performance requirements are established and preliminary designs of an integrated 'baseline' control system for single and multiengine aircraft for the 1990 operational time period are presented. Finally, stability analysis requirements and procedures are established for each of the two designs. During Phase II, detail design of the power control system will be completed and a stability analysis will be conducted. (Author)