Denna lektion utarbetades av en Local Solar System Den här artikeln är en medlem av stiftelseteamet och kan förbättras av en kvalificerad granskare. Är du kvalificerad inom det här ämnet? Föreslå en redigering
In December 1965 Gemini 6 and Gemini 7 flew within 30 centimetres of each other, 300 km above the Earth. It took two years of theory and practice to get there: the first attempts had shown that flying straight at your target, as a pilot would, does not work in orbit.
In orbit, to catch up you drop down, not speed up.
Look
Everything in orbit follows one rule: lower is faster. A lower orbit is shorter and the spacecraft moves faster along it, so it gains on anything higher up.
- Launch into a lower orbit, behind the target. The capsule is timed to start some way behind the station and slightly below it.
- Phasing. Lap after lap, the lower capsule gains a little. Here, 20 km below the station, it gains 1.6 degrees per orbit.
- Two small burns, a mini Hohmann transfer, lift the capsule into the station’s orbit just behind it.
- Final approach. The last few hundred metres are flown slowly, straight along the flight direction, by computers watched by the crew. At contact the closing speed is a few centimetres per second.
Understand
Orbital period: 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.
Each capsule orbit, the station covers only 92.6/93.0 of a lap: the capsule gains 360° × (1 − 92.6/93.0) ≈ 1.6°, about 190 km. Closing a 20° gap takes about 13 orbits, roughly 20 hours.
The transfer from 400 to 420 km costs about 5.6 m/s for each of the two burns: tiny compared with the 7.7 km/s of orbital speed.
Master
Near the target, rendezvous engineers use the Clohessy-Wiltshire (Hill) equations: linearised motion in a frame that orbits with the target, with x radial, y along-track and n the target’s mean motion:
ẍ − 3n²x − 2nẏ = 0, ÿ + 2nẋ = 0, z̈ + n²z = 0
They explain the strange behaviour: a push forwards (+ẏ) makes the chaser rise (x grows) and then drift backwards. Approach paths are designed along the y axis (V-bar, from behind) or the x axis (R-bar, from below, where the natural motion helps brake), with safety rules so that a failed engine never leads to a collision.
Prova det själv
Pretend you are the capsule, 20 degrees behind the station and at the same height. If you simply fire your engine forwards, what happens to your orbit, and do you get closer or fall further behind? (Hint: think about the Hohmann lesson.)
Utmaningar är där lärandet håller sig.
Snabb frågesport
3 snabba frågor. Välj ett svar för att se om du har rätt.
-
A capsule is behind the space station in a slightly lower orbit. Over time it:
- A Falls further behind
- B Catches up, because a lower orbit is faster
- C Stays at the same distance
- D Crashes into Earth
Visa svaret
B. Catches up, because a lower orbit is faster
-
Why can't a spacecraft just fire its engine forwards to catch a target ahead in the same orbit?
- A Because speeding up raises the orbit, which makes the lap longer, so it falls behind
- B Because engines cannot fire forwards
- C Because of air resistance
- D It can; that is how it is done
Visa svaret
A. Because speeding up raises the orbit, which makes the lap longer, so it falls behind
-
How fast does a capsule approach the station at the moment of docking?
- A About 7.7 km/s
- B About 100 m/s
- C A few centimetres per second
- D Exactly zero
Visa svaret
C. A few centimetres per second
Mållinjen
- Läs lektionen
- Gjorde utmaningen
- Gjorde frågesporten
Markera lektionen som slutförd för att spara den i dina framsteg på den här enheten.
Lektionen är klar.
Upp nästa gång Coming home: reentryOrd i den här lektionen
Källor
- 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
Denna lektion är licensierad under CC BY-SA 4.0.