Skip to main navigation Skip to search Skip to main content

Recursive Least Squares Parameter Estimation for DC Fault Detection and Localization

  • University of Dayton
  • Air Force Research Laboratory

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

6 Scopus citations

Abstract

The advancement of modern aircraft seeks to place a higher priority on the electrical power systems to execute flight operations. Transitioning to aircraft with a larger dependence on these systems is advantageous because they increase reliability, maintainability, and cost efficiency. This requires an intelligent power system that is capable of not only powering the aircraft at ideal conditions, but also detecting faults and autonomously redistributing power to flight-critical electrical loads. This paper investigates how to detect parallel faults using recursive least squares estimation. Results indicate how estimation is affected by system variables.

Original languageEnglish
Title of host publication2019 IEEE National Aerospace and Electronics Conference, NAECON 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages7-10
Number of pages4
ISBN (Electronic)9781728114163
DOIs
StatePublished - Jul 2019
Event2019 IEEE National Aerospace and Electronics Conference, NAECON 2019 - Dayton, United States
Duration: Jul 15 2019Jul 19 2019

Publication series

NameProceedings of the IEEE National Aerospace Electronics Conference, NAECON
Volume2019-July
ISSN (Print)0547-3578
ISSN (Electronic)2379-2027

Conference

Conference2019 IEEE National Aerospace and Electronics Conference, NAECON 2019
Country/TerritoryUnited States
CityDayton
Period07/15/1907/19/19

Keywords

  • DC Fault Detection
  • Intelligent Power System
  • Recursive Least Squares
  • RLS

Fingerprint

Dive into the research topics of 'Recursive Least Squares Parameter Estimation for DC Fault Detection and Localization'. Together they form a unique fingerprint.

Cite this