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| 01861cam 2200349zi 4500 |
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| 001 | 9.880795 |
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| 003 | CaOODSP |
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| 005 | 20221107165853 |
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| 006 | m o d f |
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| 007 | cr |n||||||||| |
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| 008 | 191018s1977 onc|||| o f000 0|eng d |
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| 040 | |aCaOODSP|beng|erda|cCaOODSP |
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| 043 | |an-cn--- |
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| 086 | 1 |aCo24-292/1977E-PDF |
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| 100 | 1 |aSinha, N. K.|q(Naresh Kumar),|d1927- |eauthor. |
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| 245 | 10|aReport on adaptive Kalman filtering with applications to orbital version of unified state model / |cby Naresh K. Sinha. |
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| 264 | 1|a[Ottawa] : |b[Department of Communications], |c[1977] |
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| 300 | |a1 online resource (28 pages) |
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| 336 | |atext|btxt|2rdacontent |
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| 337 | |acomputer|bc|2rdamedia |
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| 338 | |aonline resource|bcr|2rdacarrier |
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| 500 | |aDigitized edition from print [produced by Innovation, Science and Economic Development Canada]. |
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| 500 | |aCover title. |
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| 500 | |a"Submitted tothe Department of Communications under Contract Number OSU77-00165." |
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| 504 | |aIncludes bibliographical references. |
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| 520 | 3 |a"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. |
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| 650 | 0|aKalman filtering. |
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| 650 | 0|aArtificial satellites|xControl systems. |
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| 710 | 1 |aCanada. |bDepartment of Communications. |
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| 710 | 1 |aMcMaster University. |
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| 856 | 40|qPDF|s1.54 MB|uhttps://publications.gc.ca/collections/collection_2020/isde-ised/Co24/Co24-292-1977-eng.pdf |
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