Reorganized spacecraft into extras-standard. Added new ISS model from Bob
Hundley.pull/3/head
|
@ -0,0 +1,87 @@
|
|||
"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
|
||||
}
|
|
@ -0,0 +1,42 @@
|
|||
"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
|
||||
}
|
|
@ -0,0 +1,21 @@
|
|||
"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
|
||||
}
|
|
@ -0,0 +1,44 @@
|
|||
# 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
|
||||
}
|
||||
|
||||
|
After Width: | Height: | Size: 2.8 KiB |
After Width: | Height: | Size: 5.6 KiB |
After Width: | Height: | Size: 2.2 KiB |
After Width: | Height: | Size: 2.7 KiB |
After Width: | Height: | Size: 3.4 KiB |
After Width: | Height: | Size: 4.3 KiB |
After Width: | Height: | Size: 2.8 KiB |
After Width: | Height: | Size: 1.4 KiB |
After Width: | Height: | Size: 616 B |
After Width: | Height: | Size: 920 B |
After Width: | Height: | Size: 4.2 KiB |
After Width: | Height: | Size: 4.0 KiB |
After Width: | Height: | Size: 2.7 KiB |
After Width: | Height: | Size: 631 B |
After Width: | Height: | Size: 1.1 KiB |
After Width: | Height: | Size: 484 B |
After Width: | Height: | Size: 509 B |
After Width: | Height: | Size: 2.9 KiB |
After Width: | Height: | Size: 1.6 KiB |
After Width: | Height: | Size: 2.4 KiB |
After Width: | Height: | Size: 3.1 KiB |
After Width: | Height: | Size: 1.4 KiB |
After Width: | Height: | Size: 1.0 KiB |
After Width: | Height: | Size: 2.8 KiB |
After Width: | Height: | Size: 655 B |
After Width: | Height: | Size: 575 B |
After Width: | Height: | Size: 8.3 KiB |
After Width: | Height: | Size: 976 B |
After Width: | Height: | Size: 348 B |
After Width: | Height: | Size: 2.1 KiB |
After Width: | Height: | Size: 2.5 KiB |
After Width: | Height: | Size: 3.3 KiB |
After Width: | Height: | Size: 5.4 KiB |
After Width: | Height: | Size: 2.4 KiB |
After Width: | Height: | Size: 2.6 KiB |
After Width: | Height: | Size: 1.9 KiB |
|
@ -0,0 +1,28 @@
|
|||
"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
|
||||
}
|