A MODIFIED KALMAN FILTER FOR RADIO GUIDANCE APPLICATION,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1967
- Accession Number
- AD0668447
Entities
People
- J. A. Henz
Organizations
- The Aerospace Corporation