NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Utilization of landmark data in attitude/orbit determinationA mathematical model is reported for determination of satellite position, velocity, and attitude using landmark coordinates as observables. This model, although developed with respect to earth stabilized missions, Tiros-N and Nimbus-G in particular, is applicable to any earth stabilized satellite in general.
Document ID
19760003093
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Siddalingaiah, H. (Computer Sciences Corp. Silver Spring, MD, United States)
Desai, P. S. (Computer Sciences Corp. Silver Spring, MD, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
76N10181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760003079Collected WorksFlight Mechanics/Estimation Theory Symposium
No Preview Available