| Bahan Kajian | - Penerapan mekanika benda langit pada benda-benda buatan manusia yang diluncurkan ke luar angkasa; Inisialisasi Astronautica; Review Hukum Kepler dan Hukum Newton, Persamaan orbit dalam sistem dua benda dan tiga benda; Gerak jatuh bebas; Konsep Alih Orbit; Gangguan gravitasional dan non gravitasional; Orbit geosinkron dan permasalahannya
- Topik khusus: kuliah kolaborasi dengan Prodi Teknik Penerbangan dan Tenik Elektro: Mission to the Moon
| - Application of celestial body mechanics to man-made objects launched into space; Initialize Astronautica; Review of Kepler's Laws and Newton's Laws, Orbital equations in two-body and three-body systems; Free fall motion; Orbit Switch Concept; Gravitational and non-gravitational disturbances; Geosynchronous orbit and its problems
- Special topic: collaborative lecture with the Aeronautical Engineering and Electrical Engineering Study Program: Mission to the Moon
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| Capaian Pembelajaran Mata Kuliah (CPMK) | - Memahami bandwidth dan jejak, topologi jaringan, transmisi dupleks point-to-point, jaringan bintang, jaringan mesh, dan sistem penentuan posisi global (GPS).
- Memahami persamaan gerak, desain orbit, perpindahan orbit, perpindahan Hohmann, dan gerak hiperbola.
- Memahami penentuan unsur, transformasi sistem Julian ke sistem Gregorian dan sebaliknya, posisi satelit ke pengamat, metode Laplace.
- Memahami teori dasar, menarik dan menangkap gravitasi, merancang lintasan, review permasalahan tiga benda, contoh misi luar angkasa.
- Memahami teori dasar, gangguan gravitasi dan non-gravitasi, gambaran atmosfer bumi, dan model atmosfer bumi, pengaruh gerhana terhadap orbit geostasioner.
- Memahami orbit geostasioner ideal, deviasi elemen orbit, pemeliharaan stasiun, dan pengaruh gravitasi benda ketiga.
| - Comprehend the bandwidth and footprint, network topologies, point-to-point duplex transmission, star network, mesh network, and global positioning system (GPS).
- Comprehend the equation of motion, orbit design, orbit transfer, Hohmann transfer, and hyperbole motion.
- Comprehend determination of element, transformation Julian to Gregorian system and vice versa, satellite position to the observer, Laplace method.
- Comprehend the basic theory, pull and capture gravity, design trajectory, review of three-body problem, an example of the space mission.
- Comprehend the basic theory, gravitation, and non-gravitation perturbation, description of the Earth's atmosphere, and Earth's atmospheric model, eclipse influence on geostationary orbit.
- Comprehend the ideal geostationary orbit, deviation of orbital elements, station keeping, and gravitational influence of the third body.
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| Metode Penilaian | Kuis dan tugas, UTS, UAS, studi kasus dengan bobot terbesar. | Quizzes and assignments, Mid-semester exam, Final-semester exam, case studies as the greatest weight. |
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