My head filled up with questions today, so I'm trying to get a few out to the folks who know the answers.
First, Thanks to Jan for sending a copy of his presentation!
My question: We can get data about voltages coming from X, Y, and Z solar panels. I understand that X, Y, and Z are three spatial axes.
But solar panels are planes. Are the panels oriented in a particular plane (i.e. is the X panel in the X-Y plane or the X-Z plane) or do they rotate around their particular axis?
If they are fixed in one plane, is it standard for most satellites, or does it vary from satellite to satellite? If it varies, how can we tell which plane the solar panel is in?
Are the axes always in the same orientation (e.g. is the Z axis always pointed towards the Earth?)?
If there is a book or other reference for these kinds of things, please let me know.
Thanks for your thoughts!!
Steve AI9IN
On Thu, Oct 13, 2016 at 03:46:05PM -0400, [email protected] wrote:
My question: We can get data about voltages coming from X, Y, and Z solar panels. I understand that X, Y, and Z are three spatial axes.
But solar panels are planes. Are the panels oriented in a particular plane (i.e. is the X panel in the X-Y plane or the X-Z plane) or do they rotate around their particular axis?
The X panel's normal vector is aligned with the X axis of the satellite. So the X panel is parallel to the Y-Z plane.
If they are fixed in one plane, is it standard for most satellites, or does it vary from satellite to satellite? If it varies, how can we tell which plane the solar panel is in?
Coordinate axes are arbitary for each satellite. The designer of the satellite will include an axis triad on solid model drawings so others will know how the axes are labeled.
In fact, various components on the satellite, like attitude sensors (sun sensors, Earth horizon sensors, star trackers), will have their own axes in their own frames of reference. Some math is then required to map their measurements into the satellite's frame of reference, which is called the body frame.
Are the axes always in the same orientation (e.g. is the Z axis always pointed towards the Earth?)?
It depends on the attitude control system of the satellite. In the absence of control, the satellite could be pointed anywhere at any given time. If the satellite has magnets, it can align with the Earth's magnetic field, like a compass needle does. Earth observation satellites use reaction wheels or control-modement gyros to precisely control their pointing and keep their camera on one face of the satellite percisely pointed at the Earth.
If there is a book or other reference for these kinds of things, please let me know.
One of the common engineering texts that give an overview of all satellite subsystems and various design trades is _Space Mission Analysis and Design_ by Larson and Wertz. The latest edition of this book is now called _Space Mission Engineering_ by Wertz. But there are many others.
Regards, -Daniel VA3KKZ
Thank you. That makes a bunch of sense. For some reason my brain got stuck on thinking about extended solar panels like on the ISS, instead of on the side of a cube (Cubesat!).
Steve
On 2016-10-13 21:50, Daniel Kekez wrote:
On Thu, Oct 13, 2016 at 03:46:05PM -0400, [email protected] wrote:
My question: We can get data about voltages coming from X, Y, and Z solar panels. I understand that X, Y, and Z are three spatial axes.
But solar panels are planes. Are the panels oriented in a particular plane (i.e. is the X panel in the X-Y plane or the X-Z plane) or do they rotate around their particular axis?
The X panel's normal vector is aligned with the X axis of the satellite. So the X panel is parallel to the Y-Z plane.
If they are fixed in one plane, is it standard for most satellites, or does it vary from satellite to satellite? If it varies, how can we tell which plane the solar panel is in?
Coordinate axes are arbitary for each satellite. The designer of the satellite will include an axis triad on solid model drawings so others will know how the axes are labeled.
In fact, various components on the satellite, like attitude sensors (sun sensors, Earth horizon sensors, star trackers), will have their own axes in their own frames of reference. Some math is then required to map their measurements into the satellite's frame of reference, which is called the body frame.
Are the axes always in the same orientation (e.g. is the Z axis always pointed towards the Earth?)?
It depends on the attitude control system of the satellite. In the absence of control, the satellite could be pointed anywhere at any given time. If the satellite has magnets, it can align with the Earth's magnetic field, like a compass needle does. Earth observation satellites use reaction wheels or control-modement gyros to precisely control their pointing and keep their camera on one face of the satellite percisely pointed at the Earth.
If there is a book or other reference for these kinds of things, please let me know.
One of the common engineering texts that give an overview of all satellite subsystems and various design trades is _Space Mission Analysis and Design_ by Larson and Wertz. The latest edition of this book is now called _Space Mission Engineering_ by Wertz. But there are many others.
Regards, -Daniel VA3KKZ
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Daniel Kekez -
skristof＠etczone.com