Spacecraft Attitude Dyncamics and Control simulation framework with using specifically Momentum Exchange devices such as Reaction Wheel and Control Moment Gyroscope
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Updated
Aug 1, 2024 - C++
Spacecraft Attitude Dyncamics and Control simulation framework with using specifically Momentum Exchange devices such as Reaction Wheel and Control Moment Gyroscope
Developed an algorithm for Attitude Determination and control of a 1DOF 1U Cubesat.
Cubesat ADCS code written by Zarvan Movdawalla and Team, from MPSTME Mumbai.
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