Onboard sensors and associated ground based processing systems are used to maintain a well stabilized attitude for the RAE 1 in its near circular earth orbit despite the satellite's four extremely long and flexible antenna booms. Boom tip deflection pictures and central hub orientation measurements show that large boom vibrations and major attitude stability problems anticipated prior to launch have not materialized
An instrument system to acquire attitude determination data for the RAE-B spacecraft was designed an...
The NASA Lewis Research Center's Advanced Communication Technology Satellite (ACTS) was launched in ...
Gravity gradient dynamics experiments using Radio Astronomy Explorer Satellite in earth orbi
Attempts made to obtain a description of the in-orbit dynamic behavior of the RAE-B spacecraft and a...
A series of seven gravity-gradient dynamics experiments is proposed utilizing the Radio Astronomy Ex...
Numerical predictions of effective operating periods for RAE-A satellite vidicon camera used for mea...
Flexible body analog computer program and rigid body digital computer program for calculating dynami...
The RAE-2 spacecraft has been collecting radio astronomical measurements in the 25 kHz to 13 MHz fre...
The RAE-1 spacecraft inversion performed October 31, 1972 is described based upon the in-orbit dynam...
The Radio Astronomy Explorer Satellite (RAE-1), its hardware and its data processing are discussed. ...
Method for predicting times unsuitable for useful camera operation for Radio Astronomy Explorer sate...
The on-orbit structural dynamic performance of a microwave radiometer antenna for Earth science appl...
A gravity-gradient boom and a momentum wheel provides a passive, three-axis attitude control system ...
"A semipassive gravity-stabilized satellite has been observed to have large and unexpected yaw oscil...
Propagating attitude by integrating Euler's equation for rigid body motion has long been suggested f...
An instrument system to acquire attitude determination data for the RAE-B spacecraft was designed an...
The NASA Lewis Research Center's Advanced Communication Technology Satellite (ACTS) was launched in ...
Gravity gradient dynamics experiments using Radio Astronomy Explorer Satellite in earth orbi
Attempts made to obtain a description of the in-orbit dynamic behavior of the RAE-B spacecraft and a...
A series of seven gravity-gradient dynamics experiments is proposed utilizing the Radio Astronomy Ex...
Numerical predictions of effective operating periods for RAE-A satellite vidicon camera used for mea...
Flexible body analog computer program and rigid body digital computer program for calculating dynami...
The RAE-2 spacecraft has been collecting radio astronomical measurements in the 25 kHz to 13 MHz fre...
The RAE-1 spacecraft inversion performed October 31, 1972 is described based upon the in-orbit dynam...
The Radio Astronomy Explorer Satellite (RAE-1), its hardware and its data processing are discussed. ...
Method for predicting times unsuitable for useful camera operation for Radio Astronomy Explorer sate...
The on-orbit structural dynamic performance of a microwave radiometer antenna for Earth science appl...
A gravity-gradient boom and a momentum wheel provides a passive, three-axis attitude control system ...
"A semipassive gravity-stabilized satellite has been observed to have large and unexpected yaw oscil...
Propagating attitude by integrating Euler's equation for rigid body motion has long been suggested f...
An instrument system to acquire attitude determination data for the RAE-B spacecraft was designed an...
The NASA Lewis Research Center's Advanced Communication Technology Satellite (ACTS) was launched in ...
Gravity gradient dynamics experiments using Radio Astronomy Explorer Satellite in earth orbi