Difference between revisions of "Tutorial: Advanced Orbiting"

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== Hohmann transfer ==
 
== Hohmann transfer ==
Burn prograde at [[periapsis]] (or anywhere if circular) until the [[apoapsis]] reaches the desired altitude.
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{{See also||{{Wikipedia|Hohmann transfer orbit}}}}
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The '''Hohmann transfer''' is the most frequently used method of changing orbital altitudes while keeping the same [[Orbit#Inclination|inclination]]. The ending orbit may be around the same celestial body as it began or for travelling to another body, such as between [[Kerbin]] and the [[Mun]].  
  
Then, at apoapsis, burn prograde until periapsis is at the desired altitude.
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It involves first entering an [[Orbit#Eccentricity|eccentric]] orbit, then circularizing once reaching the desired orbital altitude. Thus, there are two burns to be made, ideally using engines with high thrust-to-weight ratios; low TtW can require up to 40% greater Δv from having to start earlier at less efficient points than [[apoapsis]] or [[periapsis]] are for changing orbits.
  
Burning retrograde at these same points will lower your orbit.
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To transfer from a lower orbit to higher:
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# Burn prograde at periapsis until the apoapsis reaches the desired altitude.
 +
# Upon reaching the raised apoapsis, burn prograde until periapsis rises to the desired altitude.
 +
 
 +
To transfer from higher to lower:
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# Burn retrograde at apoapsis until the periapsis reaches the desired altitude.
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# Upon reaching the lowered periasis, burn retrograde until apoapsis falls to the desired altitude.
  
 
== Bi-elliptical transfer ==
 
== Bi-elliptical transfer ==
The [[w:bi-elliptic transfer|bi-elliptic transfer]] can be more efficient (but slower) than the Hohmann transfer orbit in some cases (when going from a very tight orbit to a very large one: the ratio must be higher than ~12:1). This is because changes of speed are more efficient at low speeds (and therefore at high altitudes).
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{{See also||{{Wikipedia|Bi-elliptic transfer}}}}
* Start by burning prograde until your orbit becomes highly elliptical (the apoapsis must then be higher than both orbits).
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The '''bi-elliptic transfer''' can be more efficient (but slower) than the Hohmann transfer orbit in some cases (when going from a very tight orbit to a very large one: the ratio must be higher than ~12:1). This is because burns are more efficient at higher speeds, due to the Oberth effect (initial burn raises speed to increase efficiency, this is why the maneuver requires such a large change in orbits to be efficient).
 +
* Start by burning prograde (most efficiently at periapsis) until orbit becomes highly elliptical with the apoapsis higher than starting and desired orbits.
 
* At apoapsis, burn prograde until the periapsis reaches the altitude of your desired orbit.  
 
* At apoapsis, burn prograde until the periapsis reaches the altitude of your desired orbit.  
* Once reaching periapsis, burn retrograde until your orbit is circularized.
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* Upon reaching periapsis, burn retrograde until your orbit is circularized.
 +
 
 +
Opposite burns at these same points will lower your orbit. This can be used to enable [[aerobraking]] to lower your orbit height.
  
Opposite burns at these same points will lower your orbit. This can be used to allow you to use [[aerobraking]] to lower your orbit height.
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Check out TomPN's [https://ideone.com/EZ8UHX calculator] for when to use a Hohmann transfer or bi-elliptical transfer.
  
 
== Orbital plane alignment ==
 
== Orbital plane alignment ==
The first step in intercepting another orbiting body is to align your orbital plane with the target's orbital plane.
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An important part of intercepting another orbiting body is to align your orbital plane with the target's orbital plane.
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 +
Start by select the destination body as a target. This will show several new points on your orbit, in particular ascending node (AN) and descending node (DN). These are the points where your orbit crosses the plane of the other body's orbit. ("Ascending" is from the point of view of a prograde (eastward) orbit. If you're orbiting retrograde, your orbital plane "descends" below the other one at the "ascending" node.)
  
Next is to find the pivot point on your orbit that, when turned clockwise or counterclockwise (from the perspective of camera > ship > orbited object), will cause it to line up with the other orbit.
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Set up a maneuver node at the next one of these nodes. The maneuver you want is pure normal, in the opposite direction from the type of node it is. For the descending node, burn normal ("up", a pink triangle with a dot in the centre); for the ascending node, burn antinormal ("down", an upside-down pink triangle with radial lines and a dot in the centre). See [[Maneuver node]] to see what these symbols look like.
  
Next, find the midpoint between your prograde and retrograde motion on the horizon and point your ship toward it. Throttling prograde + 90 degrees on the horizon will cause your orbit to rotate clockwise. Prograde - 90 degrees on the horizon will rotate the orbit counterclockwise. It may take a few rotation sessions to perfect your orbit but this will allow you to match another orbital plane.
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General tips:
  
It is easier to achieve if your orbit is circular, mostly because you can line up the orbits in the map view much more easily.
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* Don't attempt to match planes anywhere other than an ascending or descending node. It won't work and you'll waste fuel trying.
 +
* It is easier to match orbital planes if your orbit is roughly the same shape (especially regarding eccentricity) as the target, mostly because you can line up the orbits in the map view much more easily.
 +
* Changing inclination is most efficient when you're moving slowly, i.e. high in the orbit. If you're aiming for a polar orbit, arrange that while you're still far away from the body rather than doing it after you've arrived. If you need precision afterwards, start with a high altitude parking orbit.
 +
* If you're merely changing orbits, for example to fulfill a "put a satellite in a particular orbit" contract, try to combine the two maneuvers by making the transfer from an ascending or descending node and adding a normal component to the burn.  Matching planes this way is highly efficient.
 +
* On the other hand, if you need to rendezvous with a body, it's often necessary to make the plane change as a mid-course correction.
  
 
== Orbit synchronization ==
 
== Orbit synchronization ==
 
In progress.
 
In progress.
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=== Bi-Elliptic Synchronization ===
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 +
#  Achieve a stable [[orbit]] around the same [[celestial body]] as the target.  If you don't know how there are [[tutorials]].
 +
#  At periapsis  adjust apoapsis so that it is equal to the target orbits apoapsis.
 +
#  At apoapsis circularize the orbit.
 +
#  At the highest Ascending or Descending node, match the orbital plane of the target orbit.
 +
#  At the point where the current orbit intersects the apoapsis of the target orbit, adjust the periapsis to match the target orbits periapsis.
 +
 +
If you additionally need to adjust the mean anomaly (crafts position within the orbit), delay the final periapsis adjustment and read the [[tutorials]].
  
 
=== The Exley maneuver ===
 
=== The Exley maneuver ===
(As of 0.17.1)
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(As of {{version|0.17.1}})
 
[[File:Orbit Synchronization how to.png|thumb|150px|A demonstration using a target planet with an orbit outside your starting planet's orbit.]]
 
[[File:Orbit Synchronization how to.png|thumb|150px|A demonstration using a target planet with an orbit outside your starting planet's orbit.]]
 +
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Named by its author, wiki user [[User:Sir_Exley|Sir Exley]], it is an approach to getting an encounter with a target planet without having a precise launch window planned by entering an eccentric orbit whose apoapsis meets the orbital path of your target and a periapsis whose altitude has a lower altitude around the sun that the target.
  
 
In order to easily meet with a target planet's sphere of influence, you will need to perform a few burns while at either the periapsis or apoapsis of your transfer orbit.
 
In order to easily meet with a target planet's sphere of influence, you will need to perform a few burns while at either the periapsis or apoapsis of your transfer orbit.
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Good luck!
 
Good luck!
  
[[Category:Tutorials|Tutorial: Advanced Orbiting]]
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[[Category:Tutorials|Advanced Orbiting]]

Revision as of 21:56, 24 May 2019

Hohmann transfer

→ See also: Hohmann transfer orbit on Wikipedia

The Hohmann transfer is the most frequently used method of changing orbital altitudes while keeping the same inclination. The ending orbit may be around the same celestial body as it began or for travelling to another body, such as between Kerbin and the Mun.

It involves first entering an eccentric orbit, then circularizing once reaching the desired orbital altitude. Thus, there are two burns to be made, ideally using engines with high thrust-to-weight ratios; low TtW can require up to 40% greater Δv from having to start earlier at less efficient points than apoapsis or periapsis are for changing orbits.

To transfer from a lower orbit to higher:

  1. Burn prograde at periapsis until the apoapsis reaches the desired altitude.
  2. Upon reaching the raised apoapsis, burn prograde until periapsis rises to the desired altitude.

To transfer from higher to lower:

  1. Burn retrograde at apoapsis until the periapsis reaches the desired altitude.
  2. Upon reaching the lowered periasis, burn retrograde until apoapsis falls to the desired altitude.

Bi-elliptical transfer

→ See also: Bi-elliptic transfer on Wikipedia

The bi-elliptic transfer can be more efficient (but slower) than the Hohmann transfer orbit in some cases (when going from a very tight orbit to a very large one: the ratio must be higher than ~12:1). This is because burns are more efficient at higher speeds, due to the Oberth effect (initial burn raises speed to increase efficiency, this is why the maneuver requires such a large change in orbits to be efficient).

  • Start by burning prograde (most efficiently at periapsis) until orbit becomes highly elliptical with the apoapsis higher than starting and desired orbits.
  • At apoapsis, burn prograde until the periapsis reaches the altitude of your desired orbit.
  • Upon reaching periapsis, burn retrograde until your orbit is circularized.

Opposite burns at these same points will lower your orbit. This can be used to enable aerobraking to lower your orbit height.

Check out TomPN's calculator for when to use a Hohmann transfer or bi-elliptical transfer.

Orbital plane alignment

An important part of intercepting another orbiting body is to align your orbital plane with the target's orbital plane.

Start by select the destination body as a target. This will show several new points on your orbit, in particular ascending node (AN) and descending node (DN). These are the points where your orbit crosses the plane of the other body's orbit. ("Ascending" is from the point of view of a prograde (eastward) orbit. If you're orbiting retrograde, your orbital plane "descends" below the other one at the "ascending" node.)

Set up a maneuver node at the next one of these nodes. The maneuver you want is pure normal, in the opposite direction from the type of node it is. For the descending node, burn normal ("up", a pink triangle with a dot in the centre); for the ascending node, burn antinormal ("down", an upside-down pink triangle with radial lines and a dot in the centre). See Maneuver node to see what these symbols look like.

General tips:

  • Don't attempt to match planes anywhere other than an ascending or descending node. It won't work and you'll waste fuel trying.
  • It is easier to match orbital planes if your orbit is roughly the same shape (especially regarding eccentricity) as the target, mostly because you can line up the orbits in the map view much more easily.
  • Changing inclination is most efficient when you're moving slowly, i.e. high in the orbit. If you're aiming for a polar orbit, arrange that while you're still far away from the body rather than doing it after you've arrived. If you need precision afterwards, start with a high altitude parking orbit.
  • If you're merely changing orbits, for example to fulfill a "put a satellite in a particular orbit" contract, try to combine the two maneuvers by making the transfer from an ascending or descending node and adding a normal component to the burn. Matching planes this way is highly efficient.
  • On the other hand, if you need to rendezvous with a body, it's often necessary to make the plane change as a mid-course correction.

Orbit synchronization

In progress.

Bi-Elliptic Synchronization

  1. Achieve a stable orbit around the same celestial body as the target. If you don't know how there are tutorials.
  2. At periapsis adjust apoapsis so that it is equal to the target orbits apoapsis.
  3. At apoapsis circularize the orbit.
  4. At the highest Ascending or Descending node, match the orbital plane of the target orbit.
  5. At the point where the current orbit intersects the apoapsis of the target orbit, adjust the periapsis to match the target orbits periapsis.

If you additionally need to adjust the mean anomaly (crafts position within the orbit), delay the final periapsis adjustment and read the tutorials.

The Exley maneuver

(As of version 0.17.1)

A demonstration using a target planet with an orbit outside your starting planet's orbit.

Named by its author, wiki user Sir Exley, it is an approach to getting an encounter with a target planet without having a precise launch window planned by entering an eccentric orbit whose apoapsis meets the orbital path of your target and a periapsis whose altitude has a lower altitude around the sun that the target.

In order to easily meet with a target planet's sphere of influence, you will need to perform a few burns while at either the periapsis or apoapsis of your transfer orbit.

Planets outside your original orbit

If you are meeting with a planet whose orbit is outside of your starting orbit, create a transfer orbit such that your apoapsis is as close as possible to your target planet's orbit.

Next, make a few orbits until the target planet is slightly in front of you when you reach your apoapsis. Begin a prograde burn until you see your orbit cross the target planet's near your apoapsis for a fraction of a second. If you overshoot, simply turn around and burn retrograde until the cross orbit is visible again. If your transfer orbit exceeds the planet's orbit, then you have gone too far, and have either missed the cross orbit, or do not have an apoapsis close enough to the target orbit to be affected by the planet's sphere of influence.

Planets inside your original orbit

If you are meeting with a planet whose orbit is inside of your starting orbit, create a transfer orbit such that your periapsis is as close as possible to your target planet's orbit.

Next, make a few orbits until the target planet is slightly behind you when you reach your periapsis. Begin a retrograde burn until you see your orbit cross the target planet's near your periapsis for a fraction of a second. If you overshoot, simply turn around and burn prograde until the cross orbit is visible again. If your transfer orbit goes within the planet's orbit, then you have gone too far, and have either missed the cross orbit, or do not have a periapsis close enough to the target orbit to be affected by the planet's sphere of influence.

Finally

Once you are in the cross orbit, burn retrograde until the orbit goes around your target planet.

Good luck!