Math problem, RotationOffset
Posted: 26.07.2005, 14:34
Well, i have struggled with this problem all day, and simply cannot solve
it. Probably because i really don??t understand the problem; i have no
math background at all. Hope someone here can show me how to solve
it - not using math symbols, which is greek to me (sorry, couldn??t help
that one):-)
Here goes:
-------------------
- I have a comet with a rotationperiod of 12 hours
- On the surface, i have a balloon. It, too, has a rotationperiod of 12 hours
to make it stand still on the surface. The balloon rotates along it??s poles, not it??s equator.
Next, we have the Earth. As the comet passes the Earth, the balloon
travels along an XYZ path from the comet surface to the Earth surface.
The trip takes 86 minutes.
Now, before takeoff, the comet stands upright on the Comet surface.
This means it arrives on Earth??s surface upside down. So, right before
takeoff, i switch the ballon model to a different SSC entry that can have it??s own RotationPeriod.
This new rotationperiod should let the balloon rotate around itself exactly one half turn
before arriving on Earth. That means it should have a rotationperiod of 2.86 hours,
but since the XYZ is attached to the comet, one has to take into account
the rotation of the comet during the flight (1.43 hours, as the XYZ
starting point will move.
So, what is the rotationperiod of the comet, to make it stand upright on
both the comet surface AND the Earth?
If anyone is interested, here??s the zipped up XYZ and SSC for the
objects - together with CelUrl??s for the start and end points of the XYZ:
http://runar.thorvaldsen.net/celestia/temp/balloondata.zip
Any help at all would be greatly appreciated; i have tried everything, and has now
resorted to experimenting wildly, which, it seems, i can do for weeks
without getting any usable result...
PS: if you wonder what this is all about, see this thread:
http://shatters.net/forum/viewtopic.php?t=7683
Thanks,
- rthorvald
it. Probably because i really don??t understand the problem; i have no
math background at all. Hope someone here can show me how to solve
it - not using math symbols, which is greek to me (sorry, couldn??t help
that one):-)
Here goes:
-------------------
- I have a comet with a rotationperiod of 12 hours
- On the surface, i have a balloon. It, too, has a rotationperiod of 12 hours
to make it stand still on the surface. The balloon rotates along it??s poles, not it??s equator.
Next, we have the Earth. As the comet passes the Earth, the balloon
travels along an XYZ path from the comet surface to the Earth surface.
The trip takes 86 minutes.
Now, before takeoff, the comet stands upright on the Comet surface.
This means it arrives on Earth??s surface upside down. So, right before
takeoff, i switch the ballon model to a different SSC entry that can have it??s own RotationPeriod.
This new rotationperiod should let the balloon rotate around itself exactly one half turn
before arriving on Earth. That means it should have a rotationperiod of 2.86 hours,
but since the XYZ is attached to the comet, one has to take into account
the rotation of the comet during the flight (1.43 hours, as the XYZ
starting point will move.
So, what is the rotationperiod of the comet, to make it stand upright on
both the comet surface AND the Earth?
If anyone is interested, here??s the zipped up XYZ and SSC for the
objects - together with CelUrl??s for the start and end points of the XYZ:
http://runar.thorvaldsen.net/celestia/temp/balloondata.zip
Any help at all would be greatly appreciated; i have tried everything, and has now
resorted to experimenting wildly, which, it seems, i can do for weeks
without getting any usable result...
PS: if you wonder what this is all about, see this thread:
http://shatters.net/forum/viewtopic.php?t=7683
Thanks,
- rthorvald