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Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.Includes bibliographical references (p. 87-89).by Pejmun Motaghedi.M.S
Attitude control of a satellite is required for the pointing of communications antennas and other in...
In this thesis we establish a framework with which to characterize candidate sources of disturbance ...
The Hubble Space Telescope features the most exacting line of sight jitter requirement thus far impo...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
This paper presents the modeling and analysis of the induced oscillations due to the Solar Array Dri...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.Mi...
This report includes: (1) introduction to mirror motion compensation (MMS); (2) EOS platform model a...
Attitude requirements of a satellite are determined by its mission: telecommunications, optical imag...
A case study, written in a tutorial manner, is presented where a comprehensive computer simulation i...
With the ever more demanding goals of space exploration and research comes the need for more complex...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
CubeSats and small satellites have become popular methods of performing space research. Accordingly,...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
In this thesis we establish a framework with which to characterize candidate sources of disturbance ...
The Hubble Space Telescope features the most exacting line of sight jitter requirement thus far impo...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
This paper presents the modeling and analysis of the induced oscillations due to the Solar Array Dri...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.Mi...
This report includes: (1) introduction to mirror motion compensation (MMS); (2) EOS platform model a...
Attitude requirements of a satellite are determined by its mission: telecommunications, optical imag...
A case study, written in a tutorial manner, is presented where a comprehensive computer simulation i...
With the ever more demanding goals of space exploration and research comes the need for more complex...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
CubeSats and small satellites have become popular methods of performing space research. Accordingly,...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
In this thesis we establish a framework with which to characterize candidate sources of disturbance ...
The Hubble Space Telescope features the most exacting line of sight jitter requirement thus far impo...
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