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Analysis of estimation algorithms for autonomous navigation with TDRSS dataEstimation techniques for onboard orbit determination using Tracking and Data Relay Satellite System (TDRSS) data are investigated. The two user satellite orbits studied are similar to Landsat-D (near-circular, 700 kilometers altitude, near-polar inclination). The following estimation algorithms are identified as candidates for use in autonomous navigation: (1) the extended Kalman filter with process noise, (2) the EKF with consider parameters, (3) the sequential Kalman filter with consider parameters, and (4) the batch least-squares differential correction technique. The candidate estimators are evaluated with respect to their performance with both baseline and worst TDRSS measurement errors and tracking configurations.
Document ID
19810002568
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dunham, J.
(Computer Sciences Corp. El Segundo, CA, United States)
Long, A.
(Computer Sciences Corp. El Segundo, CA, United States)
Gural, P.
(Computer Sciences Corp. El Segundo, CA, United States)
Preiss, K.
(Computer Sciences Corp. El Segundo, CA, United States)
Sielski, H.
(Computer Sciences Corp. El Segundo, CA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Fifth Ann. Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
81N11076
Funding Number(s)
CONTRACT_GRANT: NAS5-24300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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