Add to ORKGA weighted least-squares recursive estimator program is reported for simulating spacecraft orbital position by analyzing earth and sun sensor data. The program uses constant time adjustment for a set of ephemeris data to eliminate intrack error and to improve attitude determination accuracy
An application of a precision orbit determination technique for NASA's Earth Observing System (EOS) ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Earth Observing System (EOS) spacecraft will take measurements of the Earth's clouds, oceans, atmosp...
Methods of orbital position estimation were reviewed. The problem of accuracy in orbital mechanics i...
This paper explores using a gravity gradiometer to measure the attitude of a satellite, given that t...
Results are given of an investigation of the effects of spacecraft orbital ephemeris and attitude er...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
textSome modern spacecraft missions require precise knowledge of the attitude, obtained from the gro...
Computer simulation results of attitude estimation of Earth-orbiting satellites (including Space Tel...
An algorithm to conduct spacecraft position estimation and attitude determination via terrestrial il...
A mathematical model is reported for determination of satellite position, velocity, and attitude usi...
Precision attitude determination for recent and planned space missions typically includes quaternion...
Methods of determining satellite orbit and attitude parameters are considered. The Goddard Trajector...
This paper summarizes a compilation of attitude determination accuracies attained by a number of sat...
NASA and other space agencies have shown interest in sending humans on missions beyond low Earth orb...
An application of a precision orbit determination technique for NASA's Earth Observing System (EOS) ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Earth Observing System (EOS) spacecraft will take measurements of the Earth's clouds, oceans, atmosp...
Methods of orbital position estimation were reviewed. The problem of accuracy in orbital mechanics i...
This paper explores using a gravity gradiometer to measure the attitude of a satellite, given that t...
Results are given of an investigation of the effects of spacecraft orbital ephemeris and attitude er...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
textSome modern spacecraft missions require precise knowledge of the attitude, obtained from the gro...
Computer simulation results of attitude estimation of Earth-orbiting satellites (including Space Tel...
An algorithm to conduct spacecraft position estimation and attitude determination via terrestrial il...
A mathematical model is reported for determination of satellite position, velocity, and attitude usi...
Precision attitude determination for recent and planned space missions typically includes quaternion...
Methods of determining satellite orbit and attitude parameters are considered. The Goddard Trajector...
This paper summarizes a compilation of attitude determination accuracies attained by a number of sat...
NASA and other space agencies have shown interest in sending humans on missions beyond low Earth orb...
An application of a precision orbit determination technique for NASA's Earth Observing System (EOS) ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Earth Observing System (EOS) spacecraft will take measurements of the Earth's clouds, oceans, atmosp...