Reorganized spacecraft into extras-standard. Added new ISS model from Bob

Hundley.
pull/3/head
Chris Laurel 2008-10-06 23:41:16 +00:00
parent d805182080
commit bbb65e9ff7
49 changed files with 8025 additions and 0 deletions

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"Cassini" "Sol"
{
Class "spacecraft"
Mesh "cassini.3ds"
Radius 0.011
InfoURL "http://saturn.jpl.nasa.gov/home/index.cfm"
# Orient the model according to the specification here:
# http://mapsview.engin.umich.edu/data_descriptions/spacecraft_overview.php
# Remote sensing pallet mounted on +X side of spacecraft
# Magnetometer boom extends in +Y direction
# Primary remote sensing boresight view is -Y
# Main engine firing direction is +Z
# High-gain antenna points -Z
# Huygens probe ejected in -X direction
Orientation [ 180 1 0 0 ]
Timeline [
# Phase 1: Launch and cruise
{
Beginning "1997 10 15 09:27:11"
Ending "2004 6 20 12:00:00"
OrbitFrame { EclipticJ2000 { Center "Sol" } }
SampledTrajectory { Source "cassini-cruise.xyzv" }
FixedRotation { Inclination 70 AscendingNode -90 }
}
# Phase 2: Saturn orbit
{
#Ending "2010 7 21 12:00:00"
OrbitFrame { EclipticJ2000 { Center "Sol/Saturn" } }
SampledTrajectory { Source "cassini-orbit.xyzv" }
FixedRotation { Inclination 70 AscendingNode -90 }
}
]
}
"Huygens" "Sol/Cassini"
{
Class "spacecraft"
Mesh "huygens.3ds"
Radius 0.00135
Orientation [ 90 0 0 1 ]
InfoURL "http://saturn.jpl.nasa.gov/home/index.cfm"
Timeline [
# Phase 1: With Cassini
{
Beginning 2450736.893877314 # 1997 Oct 15 09:27:11
Ending "2004 12 25 02:01:05.183"
OrbitFrame { BodyFixed { Center "Sol/Cassini" } }
BodyFrame { BodyFixed { Center "Sol/Cassini" } }
FixedPosition [ -0.0014 0 0.0002 ]
FixedRotation { Inclination 90 AscendingNode 90 }
}
# Phase 2: Free flight to Titan
{
Ending "2005 01 14 09:07:00"
OrbitFrame { EclipticJ2000 { Center "Sol/Saturn" } }
BodyFrame { EclipticJ2000 { Center "Sol" } }
SampledTrajectory { Source "huygens.xyzv" }
UniformRotation
{
AscendingNode 0
Inclination 90
MeridianAngle 0
Epoch 2453364.5847 # 2004 Dec 25 02:01:58
Period 0.125 # 7.5 revolutions per minute
}
}
] # End Timeline
}

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"Galileo" "Sol"
{
Class "spacecraft"
Mesh "galileo.3ds"
Radius 0.01
InfoURL "http://galileo.jpl.nasa.gov"
Beginning "1989 10 19 02:47" # Launch
Ending "2003 9 21 10:44" # Crash into Jupiter
SampledOrbit "galileo.xyz"
# Use a two vector frame to keep the spacecraft's High Gain Antenna
# pointed toward the Earth. The secondary axis is chosen (arbitrarily) as
# ecliptic north.
BodyFrame {
TwoVector {
Primary {
Axis "-z"
RelativePosition {
Observer "Sol/Galileo"
Target "Sol/Earth"
}
}
Secondary {
Axis "x"
ConstantVector {
Vector [ 0 0 1 ]
Frame { EclipticJ2000 { } }
}
}
}
}
FixedRotation { }
# Orient the model so that the High Gain Antenna points in -z
# and the sensor boom points in +y
Orientation [ -90 1 0 0 ]
Albedo 0.50
}

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"Hubble" "Sol/Earth"
{
Class "spacecraft"
Mesh "hubble.cmod"
Radius 0.007 # 14 meters across
Beginning 2448007 # Deployed 25 April 1990
# Ending 2010?
EllipticalOrbit {
Period 0.06903
SemiMajorAxis 6767
Eccentricity 0.0012082
Inclination 28.4675
AscendingNode 51.0100
ArgOfPericenter 27.0378
MeanAnomaly 333.0836
Epoch 2452028.18381755
}
Albedo 0.10
}

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# International Space Station
# The model is a deconstruction of Andrew Farnaby's complete ISS model located
# on bh's website (http://www.bobhundley.com/celestia/iss.html).
#
# "New ISS" is a modification of the model that can be found here:
# http://www.celestiamotherlode.net/catalog/show_addon_details.php?addon_id=1199
# the ISS model of June 2008 (with Kibo) by krisci3 (modified in order to work
# with JPG by Ulrich Dickmann, a.k.a. Adirondack)
# All required textures by Bob Hundley (converted from BMP to JPG by
# Ulrich Dickmann)
Modify "ISS" "Sol/Earth"
{
Class "spacecraft"
Mesh "iss.cmod"
Radius 0.040
Beginning 2451138 # Zarya module launched 20 Nov 1998
EllipticalOrbit {
Period 0.064176392
SemiMajorAxis 6767
Eccentricity 0.0016886
Inclination 51.5684
AscendingNode 343.1518
ArgOfPericenter 346.2476
MeanAnomaly 13.8216
Epoch 2452028.18381755
}
UniformRotation
{
Inclination 51.5684
MeridianAngle -90
AscendingNode 343.1518
}
Orientation [ 90 0 0 1 ]
Albedo 0.10
}

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"Mir" "Sol/Earth"
{
Class "spacecraft"
Mesh "mir.3ds"
Radius 0.0165 # Mir is 33 meters long
Beginning 2446482.0 # Launched 20 Feb 1986
Ending 2451989.77083 # Reentered 21 Mar 2001
# Assuming these elements to be constant isn't accurate . . .
EllipticalOrbit {
Period 0.06415338
SemiMajorAxis 6769
Eccentricity 0.0000831
Inclination 51.6461
AscendingNode 83.8459
ArgOfPericenter 296.4901
MeanAnomaly 63.6005
}
UniformRotation
{
Inclination 51.6461
MeridianAngle 180
AscendingNode 83.8459
}
Albedo 0.10
}

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