Add to ORKGSystem design analysis to establish feasibility of using electro-optical celestial scanning sensor on IMP spacecraft for determination of spacecraft attitude by star measurement
Experimental model of infrared horizon scanner for use in spacecraft attitude determinatio
Since the dawn of the Space Age, over six thousand satellites have been launched into Earth orbit. T...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Co...
The feasibility of using the Scanning Celestial Attitude Determination System (SCADS) during Earth R...
Test facility and equipment for evaluation of optical sensors employed in celestial navigation and g...
An attitude-sensing device for space vehicles which detects the thermal radiation discontinuity at o...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1962.In...
The Attitude Determination and Control System (ADCS) is a satellite subsystem that ensures that the ...
Star field mapping technique for determining attitude of spin stabilized spacecraf
The goal of this research effort is to investigate the analysis, design, integration, testing, and v...
Scanning optical system to provide attitude and trajectory of unmanned spacecraft during orbit about...
A system was developed to determine rocket payload attitude with respect to a star field. The system...
The development of a control system to accommodate the scientific payload of the High Energy Astrono...
Attitude determination of spin-stabilized spacecraft using star mapping techniqu
Experimental model of infrared horizon scanner for use in spacecraft attitude determinatio
Since the dawn of the Space Age, over six thousand satellites have been launched into Earth orbit. T...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...
Scanning Celestial Attitude Determination System /SCADS/ for three axis attitude determination at Co...
The feasibility of using the Scanning Celestial Attitude Determination System (SCADS) during Earth R...
Test facility and equipment for evaluation of optical sensors employed in celestial navigation and g...
An attitude-sensing device for space vehicles which detects the thermal radiation discontinuity at o...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1962.In...
The Attitude Determination and Control System (ADCS) is a satellite subsystem that ensures that the ...
Star field mapping technique for determining attitude of spin stabilized spacecraf
The goal of this research effort is to investigate the analysis, design, integration, testing, and v...
Scanning optical system to provide attitude and trajectory of unmanned spacecraft during orbit about...
A system was developed to determine rocket payload attitude with respect to a star field. The system...
The development of a control system to accommodate the scientific payload of the High Energy Astrono...
Attitude determination of spin-stabilized spacecraft using star mapping techniqu
Experimental model of infrared horizon scanner for use in spacecraft attitude determinatio
Since the dawn of the Space Age, over six thousand satellites have been launched into Earth orbit. T...
Knowing a spacecraft’s orientation is crucial for many vital functions. Attitude is often determined...