Spacecraft Attitude and Orbit Control
(ECTS: 3; SWS: 2)| prerequisites | -- | |
| objectives | At the end of the module the students will be able to understand the principles of spacecraft flight dynamics including determination and control of orbit and attitude. They will be able to analyze basic properties of orbit and attitude systems and apply the basic principles for determination and control. The students will have learned how spacecrafts' trajectories and orientation are operated. | |
| contents |
Orbit Determination, including measurements, modeling, state transition matrix, parameter estimation Orbit Control, including Earth orbit, interplanetary flights and Lagrange points Attitude Determination, including the deterministic method, q-method and sensors Attitude Control, including AOCS algorithms and actuators Examples and applications from actual space missions |
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| literature |
Walter: Astronautics Sidi: Spacecraft Dynamics and Control Montenbruck/Gill: Satellite Orbits Wertz: Spacecraft Attitude Determination and Control |
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