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AE 245
Spacecraft Dynamics and Control
3
1 Reviews
Rigid body dynamics review. Attitude kinematical representations. Development and solution of general equations of motion. Single and dual-spin, zero and biased-momentum spacecraft. Control system design strategies. Common torquer elements. Computer simulations.
Prerequisite(s): BS in Aerospace Engineering or instructor consent.
3 unit(s) Units
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Average Grade
100%
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Grade: -
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Lorem ipsum dolor sit amet, consectetur adipiscing elit. Nullam nec purus nec libero ultricies lacinia. Nullam nec purus nec libero ultricies lacinia.
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