[amsat-bb] Re: some exceedingly clever technology

2011-08-29 Thread Terry Carrell

This is what the KiwiSAT - ADAC - experiment will investigate.
http://www.kiwisat.org/science.html

Terry, ZL3QL.

- Original Message - 
From: Phil Karn k...@philkarn.net

To: R Oler orbit...@hotmail.com
Cc: Amsat BB 
Sent: Saturday, August 27, 2011 4:54 AM
Subject: [amsat-bb] Re: some exceedingly clever technology



On 8/24/11 8:11 PM, R Oler wrote:


http://onorbit.com/node/3709


Thrusters are necessary for orbit control, but for attitude control
(which I think we really need) you'd *really* prefer something that
doesn't consume a fuel.

These attitude control systems come in basically two types:
magnetorquers and reaction wheels. Magnetorquers exchange angular
momentum with the earth by acting on its magnetic field, but they tend
to be slow, imprecise and require complex control and sensing systems
including a magnetometer far enough from the spacecraft to get away from
its own magnetic fields.

Reaction wheels come in two kinds: momentum wheels and control moment
gyros. Momentum wheels change speed while control moment gyros don't.
The latter seem much more common in spacecraft but I'd investigate both.
They're good for quick, accurate pointing like you'd need to keep an
antenna pointed down or a solar panel pointed at the sun.

Having both a magnetorquer and a set of wheels can be advantageous as
the magnetorquer can be used occasionally to dump accumulated angular
momentum from the wheels should it build up from small external torques.

Controlling attitude also means measuring it, and for this I keep
thinking about small, cheap CCD video cameras. If we could build good
enough sunshades we could snap pictures of star fields and look them up
in a database. If you can match multiple stars in an image, then a
single image could fix the attitude of the spacecraft. But I'd want to
put a camera on each surface if possible. They could also sense the sun
and the earth, though that's not as simple as it might seem. The sun
usually overloads a CCD and produces streaks while the earth is very
large in LEO. It might be possible to recognize the limb of the earth
and get better precision that way. A lot would depend on the software
processing these images, and it would be a challenge to write.

-Phil, KA9Q

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[amsat-bb] Re: some exceedingly clever technology

2011-08-27 Thread i8cvs
Hi Phil, KA9Q

What you describes using both magnetorquers ,momentum wheels
and CCD video cameras for the attitude control system is what
was made on AO40 but it was a big satellite and not a microsatellite.

73 de

i8CVS Domenico

- Original Message -
From: Phil Karn k...@philkarn.net
To: R Oler orbit...@hotmail.com
Cc: Amsat BB amsat-bb@amsat.org
Sent: Friday, August 26, 2011 6:54 PM
Subject: [amsat-bb] Re: some exceedingly clever technology


 On 8/24/11 8:11 PM, R Oler wrote:
 
  http://onorbit.com/node/3709

 Thrusters are necessary for orbit control, but for attitude control
 (which I think we really need) you'd *really* prefer something that
 doesn't consume a fuel.

 These attitude control systems come in basically two types:
 magnetorquers and reaction wheels. Magnetorquers exchange angular
 momentum with the earth by acting on its magnetic field, but they tend
 to be slow, imprecise and require complex control and sensing systems
 including a magnetometer far enough from the spacecraft to get away from
 its own magnetic fields.

 Reaction wheels come in two kinds: momentum wheels and control moment
 gyros. Momentum wheels change speed while control moment gyros don't.
 The latter seem much more common in spacecraft but I'd investigate both.
 They're good for quick, accurate pointing like you'd need to keep an
 antenna pointed down or a solar panel pointed at the sun.

 Having both a magnetorquer and a set of wheels can be advantageous as
 the magnetorquer can be used occasionally to dump accumulated angular
 momentum from the wheels should it build up from small external torques.

 Controlling attitude also means measuring it, and for this I keep
 thinking about small, cheap CCD video cameras. If we could build good
 enough sunshades we could snap pictures of star fields and look them up
 in a database. If you can match multiple stars in an image, then a
 single image could fix the attitude of the spacecraft. But I'd want to
 put a camera on each surface if possible. They could also sense the sun
 and the earth, though that's not as simple as it might seem. The sun
 usually overloads a CCD and produces streaks while the earth is very
 large in LEO. It might be possible to recognize the limb of the earth
 and get better precision that way. A lot would depend on the software
 processing these images, and it would be a challenge to write.

 -Phil, KA9Q

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 Not an AMSAT-NA member? Join now to support the amateur satellite program!
 Subscription settings: http://amsat.org/mailman/listinfo/amsat-bb

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[amsat-bb] Re: some exceedingly clever technology

2011-08-26 Thread Gregg Wonderly
This is exactly the kind of low tech solution that we need to use in amateur 
sats to have orientation and orbital control.  But, I worry that if we did 
demonstrate control, would we be allowed to be in control since the craft 
could then become a weapon in the hands of the wrong person.


Gregg
W5GGW

On 8/24/2011 10:11 PM, R Oler wrote:


http://onorbit.com/node/3709

Robert G. Oler WB5MZO Life member AMSAT ARRL NARS

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[amsat-bb] Re: some exceedingly clever technology

2011-08-26 Thread Phil Karn
On 8/24/11 8:11 PM, R Oler wrote:
 
 http://onorbit.com/node/3709  

Thrusters are necessary for orbit control, but for attitude control
(which I think we really need) you'd *really* prefer something that
doesn't consume a fuel.

These attitude control systems come in basically two types:
magnetorquers and reaction wheels. Magnetorquers exchange angular
momentum with the earth by acting on its magnetic field, but they tend
to be slow, imprecise and require complex control and sensing systems
including a magnetometer far enough from the spacecraft to get away from
its own magnetic fields.

Reaction wheels come in two kinds: momentum wheels and control moment
gyros. Momentum wheels change speed while control moment gyros don't.
The latter seem much more common in spacecraft but I'd investigate both.
They're good for quick, accurate pointing like you'd need to keep an
antenna pointed down or a solar panel pointed at the sun.

Having both a magnetorquer and a set of wheels can be advantageous as
the magnetorquer can be used occasionally to dump accumulated angular
momentum from the wheels should it build up from small external torques.

Controlling attitude also means measuring it, and for this I keep
thinking about small, cheap CCD video cameras. If we could build good
enough sunshades we could snap pictures of star fields and look them up
in a database. If you can match multiple stars in an image, then a
single image could fix the attitude of the spacecraft. But I'd want to
put a camera on each surface if possible. They could also sense the sun
and the earth, though that's not as simple as it might seem. The sun
usually overloads a CCD and produces streaks while the earth is very
large in LEO. It might be possible to recognize the limb of the earth
and get better precision that way. A lot would depend on the software
processing these images, and it would be a challenge to write.

-Phil, KA9Q

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