The goal of this capstone spacecraft dynamics project is to employ the skills developed in the rigid body Kinematics, Kinetics and Control courses. An exciting two-spacecraft mission to Mars is considered where a primary mother craft is in communication with a daughter vehicle in another orbit. The challenges include determining the kinematics of the orbit frame and several desired reference frames, numerically simulating the attitude dynamics of the spacecraft in orbit, and implementing a feedback control that then drives different spacecraft body frames to a range of mission modes including sun pointing for power generation, nadir pointing for science gathering, mother spacecraft pointing for communication and data transfer. Finally, an integrated mission simulation is developed that implements these attitude modes and explores the resulting autonomous closed-loop performance.
À propos de ce cours
Université du Colorado à Boulder
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- 5 stars80 %
- 4 stars15 %
- 3 stars2,50 %
- 1 star2,50 %
Meilleurs avis pour SPACECRAFT DYNAMICS CAPSTONE: MARS MISSION
Great application of the knowledge obtained through the course
Excellent, comprehensive review of the course - kinetics, kinematics, and control but I removed a star due to the tight tolerances in the answers. I was off by exactly 0.001 and it was marked wrong.
À propos du Spécialisation Spacecraft Dynamics and Control
Spacecraft Dynamics and Control covers three core topic areas: the description of the motion and rates of motion of rigid bodies (Kinematics), developing the equations of motion that prediction the movement of rigid bodies taking into account mass, torque, and inertia (Kinetics), and finally non-linear controls to program specific orientations and achieve precise aiming goals in three-dimensional space (Control). The specialization invites learners to develop competency in these three areas through targeted content delivery, continuous concept reinforcement, and project applications.
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