Accession Number:

AD0668447

Title:

A MODIFIED KALMAN FILTER FOR RADIO GUIDANCE APPLICATION,

Descriptive Note:

Corporate Author:

AEROSPACE CORP EL SEGUNDO CALIF

Personal Author(s):

Report Date:

1967-12-01

Pagination or Media Count:

131.0

Abstract:

The modified Kalman filtering technique offers several distinct advantages over filters used previously in radio guidance equations. Presented are a derivation of the Kalman filter the filter force, measurement, and noise models the transition matrix and coordinate transformation matrix derivations a description of the modified filter equations and results obtained from a computer program using the modified filter equations. Author

Subject Categories:

  • Cybernetics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE