Kode Mata KuliahAS3207 / 3 SKS
Penyelenggara103 - Astronomy / FMIPA
KategoriLecture
Bahasa IndonesiaEnglish
Nama Mata KuliahLintasan SatelitSatellite Orbits
Bahan Kajian
  1. 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
  2. Topik khusus: kuliah kolaborasi dengan Prodi Teknik Penerbangan dan Tenik Elektro: Mission to the Moon
  1. 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
  2. Special topic: collaborative lecture with the Aeronautical Engineering and Electrical Engineering Study Program: Mission to the Moon
Capaian Pembelajaran Mata Kuliah (CPMK)
  1. Memahami bandwidth dan jejak, topologi jaringan, transmisi dupleks point-to-point, jaringan bintang, jaringan mesh, dan sistem penentuan posisi global (GPS).
  2. Memahami persamaan gerak, desain orbit, perpindahan orbit, perpindahan Hohmann, dan gerak hiperbola.
  3. Memahami penentuan unsur, transformasi sistem Julian ke sistem Gregorian dan sebaliknya, posisi satelit ke pengamat, metode Laplace.
  4. Memahami teori dasar, menarik dan menangkap gravitasi, merancang lintasan, review permasalahan tiga benda, contoh misi luar angkasa.
  5. Memahami teori dasar, gangguan gravitasi dan non-gravitasi, gambaran atmosfer bumi, dan model atmosfer bumi, pengaruh gerhana terhadap orbit geostasioner.
  6. Memahami orbit geostasioner ideal, deviasi elemen orbit, pemeliharaan stasiun, dan pengaruh gravitasi benda ketiga.
  1. Comprehend the bandwidth and footprint, network topologies, point-to-point duplex transmission, star network, mesh network, and global positioning system (GPS).
  2. Comprehend the equation of motion, orbit design, orbit transfer, Hohmann transfer, and hyperbole motion.
  3. Comprehend determination of element, transformation Julian to Gregorian system and vice versa, satellite position to the observer, Laplace method.
  4. Comprehend the basic theory, pull and capture gravity, design trajectory, review of three-body problem, an example of the space mission.
  5. 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.
  6. Comprehend the ideal geostationary orbit, deviation of orbital elements, station keeping, and gravitational influence of the third body.
Metode PembelajaranKombinasi ceramah, diskusi kelompok, dan studi kasusCombination of lectures, group discussions and case studies
Modalitas PembelajaranBauran sinkron dan asinkronSynchronous and asynchronous
Jenis NilaiABCDE
Metode PenilaianKuis dan tugas, UTS, UAS, studi kasus dengan bobot terbesar.Quizzes and assignments, Mid-semester exam, Final-semester exam, case studies as the greatest weight.
Catatan Tambahan