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The Design and Validation of a Spacecraft Orbit and Attitude Simulation Environment in MATLAB/Simulink
DownloadFall 2018
CubeSats and Aerodynamic Attitude and Orbit Control Systems (AAOCS) orbit in Very Low Earth Orbit (VLEO) where the effect of aerodynamic force and torque is significant. In the mission analysis and design phases of CubeSat missions and satellite missions employing AAOCS, aerodynamic...
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