Bab iki digawé déning Local Solar System Anggota tim Foundation bisa dioptimalkeun ku hiji reviewer anu qualified. Apa sampeyan duwe kualifikasi ing topik iki? Suggestion an edit
In December 1965 Gemini 6 and Gemini 7 flew within 30 centimetres of each other, 300 km above the Earth. Diperlukeun dua taun teori jeung prakték pikeun ngahontal éta: usaha munggaran parantos nunjukkeun yén terbang langsung ka target anjeun, sapertos pilot bakal henteu damel dina orbit.
Nalika orbit, nalika orbit, nalika orbit, nalika orbit, nalika orbit.
Lihat
Sekabeh ing orbit ngetutake siji aturan: lower is faster. Orbit anu langkung handap langkung pondok, sareng pesawat ruang angkasa gerak gancang di sakurilingna, janten gains dina naon waé anu langkung luhur.
- Launching into lower orbit, behind the target. Kapsul dijadwalkeun pikeun ngamimitian sababaraha jarak hareup stasiun sarta sakedik handapeun éta.
- Pasang. Nalika dijupuk, kapsul iki bisa dibuwang. Here, 20 km below the station, it gains 1.6 degrees per orbit.
- DurungSanggeus dioperasikeun, kapsul bakal diturunkeun ka orbit saterusna.
- Kesimpulan. Satengah jam sanggeus pesawat diluncurkeun, éta ngaleupaskeun sinyal ka awak pesawat pikeun ngumumkeun kadatangan. At contact the closing speed is a few centimetres per second.
Ngerti
Periode orbital: T = 2π√(r³/μ). With μ = 398,600 km³/s²:
- Capsule at 400 km (r = 6,778 km): 92.6 minutes.
- Station at 420 km (r = 6,798 km): 93.0 minutes.
Saben orbit kapsul, stasiun iki mung nutupi 92.6/93.0 saka hiji lap: kapsul bisa ngasilake 360° × (1 − 92.6/93.0) ≈ 1.6°, kira-kira 190 km. Closing a 20° gap takes about 13 orbits, roughly 20 hours.
Transfer saka 400 kanggo 420 km regane udakara 5.6 m/s Pikeun unggal dua burns: leutik dibandingkeun jeung 7.7 km / s tina kecepatan orbit.
Master
Ing cedhak target, insinyur rendezvous nggunakake Clohessy-Wiltshire (Hill) persamaan: linearized gerakan ing aframe sing orbit karo target, karo x radial, y along-track lan n target rata-rata gerakan:
ym − 3n²x − 2nẏ = 0, ÿ + 2nʒ = 0, z̈ + n²z = 0
They explain the strange behaviour: a push forwards (+ẏ) makes the chaser rise (x grows) and then drift backwards. Jalan pendekatan diwangun sapanjang poros y (V-bar, ti tukang) atanapi poros x (R-bar, ti handap, dimana gerak alami ngabantosan rem), sareng aturan kaamanan supados mesin anu gagal henteu pernah nyababkeun tabrakan.
Coba
Ngarasakeun anjeun kapsul, 20 derajat di tukang stasiun sareng dina luhur anu sami. Upami anjeun ngan ukur ngaleupaskeun mesin anjeun ka hareup, naon anu lumangsung kana orbit anjeun, sareng naha anjeun langkung caket atanapi langkung jauh? (Ceuk: pikirkeun ngeunaan pelajaran Hohmann.)
Great. Tantangan iku ngendi learning sticks.
Tes Cepat
3 pitakon cepet. Pilih jawaban kanggo ndeleng apa sampeyan bener.
-
Sabuah kapsul ana ing mburi stasiun luar angkasa ing orbit sing kurang luwih ngisor. Nalikane:
- A Tetep
- B Nglewati, amarga orbit sing luwih endhek luwih cepet
- C Tetep ing jarak sing padha
- D Kacau ing Bumi
Papar jawaban
B. Nglewati, amarga orbit sing luwih endhek luwih cepet
-
Nalika pesawat ruang angkasa nuju orbit, éta bisa ngaleupaskeun bahan bakar kanggo nyetir pesawat ka arah anu dituju.
- A Amargi ngetik kacepetan ngalebet orbit, ingkang ndamel lap langkung panjang, makaten punika ical
- B Sebab mesin ora bisa ngambang maju
- C Asil saka perlawanan udara
- D Bisa; kaya mangkono carane
Papar jawaban
A. Amargi ngetik kacepetan ngalebet orbit, ingkang ndamel lap langkung panjang, makaten punika ical
-
Kecepatan kapsul menyang stasiun nalika docking?
- A Kira-kira 7.7 km/s
- B 100 m/s
- C A few centimeters per second
- D Tepat nol
Papar jawaban
C. A few centimeters per second
Baris pungkasan
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Latihan rampung. Bagus!
Nganti sabanjure Coming home: reentryKata ing pelajaran iki
Sumber
- NASA, Rendezvous and docking (Gemini 6 and 7, the first space rendezvous, 1965)
- ESA, Automated Transfer Vehicle rendezvous and docking
- W. H. Clohessy and R. S. Wiltshire, Terminal Guidance System for Satellite Rendezvous (1960), J. Aerospace Sciences 27(9)
- JPL SSD, Astrodynamic parameters
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