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.
Utilization of landmark data in attitude/orbit determination
1975-08-01
Conference paper
No indication
English
Orbit/attitude estimation with LANDSAT Landmark data
NTRS | 1979
|Orbit and attitude state recoveries from Landmark data
NTRS | 1975
|Orbit and attitude state recoveries from Landmark data
NTRS | 1975
|