Report on adaptive Kalman filtering with applications to orbital version of unified state model / by Naresh K. Sinha.: Co24-292/1977E-PDF
"A sequential estimator for suboptimal adaptive estimation of the unknown a priori state and observation noise statistics simultaneously with the system state, is applied to the estimation of the states of synchronous orbit satellite. Some tracking data supplied by the CRC have been used as real observations. Results of simulation are presented, using this approach with Altman's unified state model of the orbital trajectory and the corresponding observation model"--Abstract.
Permanent link to this Catalogue record:
publications.gc.ca/pub?id=9.880795&sl=0
| Department/Agency | Canada. Department of Communications. McMaster University. |
|---|---|
| Title | Report on adaptive Kalman filtering with applications to orbital version of unified state model / by Naresh K. Sinha. |
| Publication type | Monograph |
| Language | [English] |
| Format | Electronic |
| Electronic document | |
| Note(s) | Digitized edition from print [produced by Innovation, Science and Economic Development Canada]. Cover title. "Submitted tothe Department of Communications under Contract Number OSU77-00165." Includes bibliographical references. |
| Publishing information | [Ottawa] : [Department of Communications], [1977] |
| Author / Contributor | Sinha, N. K.(Naresh Kumar),1927- author. |
| Description | 1 online resource (28 pages) |
| Catalogue number |
|
| Subject terms | Kalman filtering. Artificial satellites -- Control systems. |