Optimal Fuel System Estimation.

Abstract

The application of Kalman (Linear Least Squares Recursive) filtering to the estimation of fuel quantity and fuel rate for fighter aircraft is discussed. Error analyses are presented for the resultant filter. The 'blending' of quantity and rate information is shown to offer a tradeoff between required system accuracies and individual sensor accuracies. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 30, 1970
Accession Number
AD0717640

Entities

People

  • Nelson R. Zagalsky

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Blending
  • Error Analysis
  • Errors
  • Fighter Aircraft
  • Filters
  • Filtration
  • Fuel Systems
  • Military Aircraft

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Aerospace Engineering