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{{Addon|
 
{{Addon|
1=[http://users.kymp.net/p501474a/Orbiter/Orbiter.html IMFD]|
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1=[http://koti.mbnet.fi/jarmonik/Orbiter.html IMFD]|
 
2=[[Jarmo Nikkanen]]
 
2=[[Jarmo Nikkanen]]
 
}}
 
}}
  
'''Interplanetary MFD''' (IMFD) is an [[Orbiter]] add-on created by Jarmo Nikkanen. It facilitates travel throughout the solar system by calculating and displaying a vessel's predicted trajectory. It is first released in 2002. The complete IMFD Manual has been added to this Wiki [[IMFD Manual|here]].
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'''Interplanetary MFD''' (IMFD) is an [[Orbiter]] add-on created by Jarmo Nikkanen. It facilitates travel throughout the solar system by calculating and displaying a vessel's predicted trajectory. It is first released in 2002.
  
  
 
==Status==
 
==Status==
The current version is IMFD 5.1m released on June 26, 2008.
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The current version is IMFD 5.1g released on March 28, 2008.
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==Key Features:==
 
==Key Features:==
 
* '''Map''' program can be used to display entire solar system and predict the actual course of the vessel with numerical trajectory calculator. The predictor can be also used to predict a hypothetical scenarios as well. This is very useful when planning a free-return trajectories.
 
* '''Map''' program can be used to display entire solar system and predict the actual course of the vessel with numerical trajectory calculator. The predictor can be also used to predict a hypothetical scenarios as well. This is very useful when planning a free-return trajectories.
 
* '''Course''' program is a collection of minor navigation programs those will let you to navigate through the solar system to other planets, moons and comets. Primary programs are based on the Lambert solver. In the most simplest case only a date of ejection and the Date of arrival is required as an user input.
 
* '''Course''' program is a collection of minor navigation programs those will let you to navigate through the solar system to other planets, moons and comets. Primary programs are based on the Lambert solver. In the most simplest case only a date of ejection and the Date of arrival is required as an user input.
* '''BaseApproach''' program is designed for Apollo style Moon to Earth return missions. It can be used to target a bases on the Moon and land directly without an orbit insertion. The program will also allow to establish an orbit right over a specific base on a planet so that it is possible to continue the descent on the base. That's very useful when landing on the Moon.
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* '''BaseApproach''' program is designed for Apollo style Moon to Earth return missions. It can be used to target a bases on the Mars and land directly without an orbit insertion. The program will also allow to establish an orbit right over a specific base on a planet so that it is possible to continue the descent on the base. That's very useful when landing on the Moon.
* '''Surface Launch''' program is useful when starting interplanetary or lunar missions from the planet surface. The program will compute the time to launch window and required launch heading. This program is the only one that doesn't compute any burn guidance data. A vessel specific ascent profile should be used to reach low orbit.
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* '''Surface Launch''' program is usefull when starting interplanetary or lunar missions from the planet surface. The program will compute the time to launch window and required launch heading. This program is the only one that doesn't compute any burn guidance data. A vessel specific ascent profile should be used to reach low orbit.
 
* '''Orbit Eject''' program is required when starting interplanetary missions from the orbit. This program is used in a combination with the other programs to convert the Escape information into burn guidance data.
 
* '''Orbit Eject''' program is required when starting interplanetary missions from the orbit. This program is used in a combination with the other programs to convert the Escape information into burn guidance data.
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==General Information==
 
==General Information==
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* Map: Hyperbola position bug fixed.
 
* Map: Hyperbola position bug fixed.
 
* Ellipse draw fixed
 
* Ellipse draw fixed
* Orbital program added:
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Orbital program added:
:* Circulate orbit at any point
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* Circulate orbit at any point
:* Velocity Match
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* Velocity Match
:* Find Target
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* Find Target
  
 
====0.7====
 
====0.7====
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:When using IMFD with Apollo "AB Throttle Down" setting can be decreased down to 1 from configuration menu.
 
:When using IMFD with Apollo "AB Throttle Down" setting can be decreased down to 1 from configuration menu.
  
===5.1j (June 22, 2008)===
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==Future==
* Orbit Insert fixed
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====5.2====
 
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* TODO: Apollo TLI, TEI program (auto-offset) (work in progress)
===5.1k (June 25, 2008)===
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* TODO: Orbit Insert Fix
* Rebuild of All Libraries
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* TODO: Copy fuel-efficiency code from 5.1g
 
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* TODO: Attitude Control problems in rdenny Europa->Callisto scenario
===5.1m (June 26, 2008)===
 
* Static Linking
 
 
 
===5.2 (unknown)===
 
* Added NASSP page to display some additional info, Fixed typo from TrA
 
* Added P30 Compensation Mode selector in configuration page
 
* Fixed IPC allocation conflict with LTMFD
 
* Orbit Insert bug with Elliptical source orbits fixed
 
 
 
===5.3 (May 15, 2009)===
 
* Tangential Transfer program restored
 
* MJD tuning rate bug fixed form tangential transfer
 
 
 
==Requested Features==
 
 
 
* Escape Vector output in Delta Velocity
 
* Restore Orbital/Plane-Change
 
* Restore Orbital/Orbit-Match
 
* Lagrange Targets
 
 
 
== See also ==
 
[[IMFD Manual]]
 
 
 
  
 
==External Links==
 
==External Links==
 
http://koti.mbnet.fi/jarmonik/sc2.gif
 
http://koti.mbnet.fi/jarmonik/sc2.gif
  
[http://users.kymp.net/p501474a/Orbiter/Orbiter.html Jarmo Nikkanen's Orbiter page]
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[http://koti.mbnet.fi/jarmonik/Orbiter.html Jarmo Nikkanen's Orbiter page]
  
[[Category:Articles]]
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[[Category:Add-ons]][[Category:MFD add-ons]]
[[Category:Add-ons]]
 
[[Category:Utilities add-ons]]
 
[[Category:MFD]]
 
[[Category:MFD add-ons]]
 

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