151-0106-00L
Orbital Dynamics
| Semester | Spring Semester 2019 |
| Lecturers | A. A. Kubik |
| Periodicity | yearly recurring course |
| Language of instruction | English |
Courses
| Number | Title | Hours | | Lecturers |
|---|
| 151-0106-00 G | Orbital Dynamics | 3 hrs | | A. A. Kubik |
Catalogue data
| Abstract | Principles of the motion of natural and artificial satellites, rocket dynamics, orbital maneuvers and interplanetary missions. |
| Learning objective | Knowledge of the basic theory of satellite dynamics. Ability to apply the acquired theory to simple examples. |
| Content | The two-body problem, rocket dynamics, orbital maneuvers, interplanetary missions, the restricted three-body problem, perturbation equations, satellite attitude dynamics. |
Performance assessment
| Performance assessment information (valid until the course unit is held again) |
Performance assessment as a semester course |
| ECTS credits | 4 credits |
| Examiners | A. A. Kubik |
| Type | end-of-semester examination |
| Language of examination | English |
| Repetition | A repetition date will be offered in the first two weeks of the semester immediately consecutive. |
| Additional information on mode of examination | schriftlich 90 Minuten |
Learning materials
| No public learning materials available. |
| Only public learning materials are listed. |
Groups
| No information on groups available. |
Restrictions
| There are no additional restrictions for the registration. |
Offered in
