| Kode Mata Kuliah | AE4034 / 3 SKS |
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| Penyelenggara | 136 - Teknik Dirgantara / FTMD |
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| Kategori | Kuliah |
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| Bahasa Indonesia | English |
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| Nama Mata Kuliah | Astrodinamika | Astrodynamics |
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| Bahan Kajian | - Pengantar Astrodinamika (N-body Problem)
- Masalah Orbit Dua Benda (termasuk Initial Value Problem)
- Manuver Orbit Operasional (termasuk Rendezvous)
- Analisis Interplanetary Trajectory (termasuk Gravity assist)
- Pengantar Perturbasi Orbit
- Masalah Tiga benda Terbatas
| - Introduction to Astrodynamics (N-body Problem)
- Two-Object Orbit Problems (including Initial Value Problem)
- Operational Orbit Maneuvers (including Rendezvous)
- Interplanetary Trajectory Analysis (including Gravity assist)
- Introduction to Orbit Perturbations
- Three-Boundary Object Problem
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| Capaian Pembelajaran Mata Kuliah (CPMK) | - Menganalisis orbit dan lintasan wahana antariksa menggunakan pendekatan masalah dua benda
- Merancang manuver orbit untuk misi mengorbit Bumi dan lintasan antar planet
- Mengetahui dan mensimulasikan pengaruh gangguan orbit
- Memahami aplikasi pendekatan Masalah Tiga Benda Terbatas
| - Analyze spacecraft orbits and trajectories using the two-body problem approach.
- Design orbital maneuvers for Earth-orbiting missions and interplanetary trajectories.
- Understand and simulate the effects of orbital perturbations.
- Comprehend the application of the Restricted Three-Body Problem approach.
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| Metode Pembelajaran | Kuliah Tatap muka dan diskusi
Presentasi Tugas | |
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| Modalitas Pembelajaran | Luring Sinkron | |
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| Jenis Nilai | ABCDE |
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| Metode Penilaian | Tugas-tugas
Ujian Tengah Semester
Ujian Akhir Semester | |
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| Catatan Tambahan | | |
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