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A 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
Various important aspects of the satellite orbit determination problem are critically discussed with...
The NASA-NEEDS program goals present a requirement for on-board signal processing to achieve user-co...
This paper summarizes a compilation of attitude determination accuracies attained by a number of sat...
Currently on NOAA/NESS's VIRGS system at the World Weather Building star images are being ingested o...
Spacecraft state estimation and the absolute registration of Earth images acquired by cameras onboar...
An artificial satellite orbit determination (OD) computer program is the most essential tool in sate...
A weighted least-squares recursive estimator program is reported for simulating spacecraft orbital p...
Methods of determining satellite orbit and attitude parameters are considered. The Goddard Trajector...
The application of GPS to spacecraft attitude determination is a new and growing field. Although the...
An algorithm to conduct spacecraft position estimation and attitude determination via terrestrial il...
All spacecraft require attitude determination at some level of accuracy. This can be a very coarse r...
The configuration of satellite network systems is based on the quantities and properties related to ...
While the use of relative orbit determination has reduced the difficulties inherent in tracking geos...
Tools used in the measurement of satellite attitude are described. Attention is given to the element...
A software system is described which provides for batch least squares estimation of spacecraft orbit...
Various important aspects of the satellite orbit determination problem are critically discussed with...
The NASA-NEEDS program goals present a requirement for on-board signal processing to achieve user-co...
This paper summarizes a compilation of attitude determination accuracies attained by a number of sat...
Currently on NOAA/NESS's VIRGS system at the World Weather Building star images are being ingested o...
Spacecraft state estimation and the absolute registration of Earth images acquired by cameras onboar...
An artificial satellite orbit determination (OD) computer program is the most essential tool in sate...
A weighted least-squares recursive estimator program is reported for simulating spacecraft orbital p...
Methods of determining satellite orbit and attitude parameters are considered. The Goddard Trajector...
The application of GPS to spacecraft attitude determination is a new and growing field. Although the...
An algorithm to conduct spacecraft position estimation and attitude determination via terrestrial il...
All spacecraft require attitude determination at some level of accuracy. This can be a very coarse r...
The configuration of satellite network systems is based on the quantities and properties related to ...
While the use of relative orbit determination has reduced the difficulties inherent in tracking geos...
Tools used in the measurement of satellite attitude are described. Attention is given to the element...
A software system is described which provides for batch least squares estimation of spacecraft orbit...
Various important aspects of the satellite orbit determination problem are critically discussed with...
The NASA-NEEDS program goals present a requirement for on-board signal processing to achieve user-co...
This paper summarizes a compilation of attitude determination accuracies attained by a number of sat...
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