By shining a precisely tuned laser through an atomic vapor, we can determine local mag- netic field strength in scalar form and in a way that is not affected by temperature changes. This technology has been used in space many times before on missions flown by NASA and ESA, such as SWARM, Øersted, and CHAMP to calibrate accompanying vector mag- netometers which are subject to offsets caused by temperature changes. The device we constructed is a small, low-cost application of this scientific principle and opens up new areas of scientific possibility for cubesats and the ability to define geomagnetic field struc- tures on a small (<10km) scale as part of the ANDESITE cubesat mission being developed at Boston University. Previously, ...
Magnetometer is simple to operate and has fast response. Transducer is rugged and flat and can measu...
CubeSats are being increasingly specified for demanding Earth observation and astronomical applicati...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83632/1/AIAA-2010-7518-617.pd
A new sensor for measuring low-amplitude magnetic fields that is ideal for small spacecraft is pres...
We present the first in-flight results from a novel miniaturised anisotropic magnetoresistive space...
In the nearly two decades that CubeSats have been in significant use, over 800 have been launched, a...
A magnetometer board intended for CubeSat applications is presented. The board contains four PNI RM3...
For millennia, phenomena of the magnetosphere have intrigued mankind. Studies of the geomagnetic fie...
This report presents the development of a magnetic sensor for use onboard a nano-satellite; it woul...
Motivated by small-scale auroral plasma science, ANDESITE, a 6U CubeSat with eight deployable picosa...
Some space missions require a thorough control of the spacecraft’s magnetic environment. With the ai...
The on board resources, needed to perform the mission tasks, are very limited in nano-satellites. Th...
Researchers from the University of Michigan (UM) and NASA Goddard Spaceflight Center (GSFC) are part...
Space weather research is data-starved and small satellites offer an opportunity to the community. O...
ADCS magnetometers on board of satellites suffer from the disruptive magnetic field produced by the ...
Magnetometer is simple to operate and has fast response. Transducer is rugged and flat and can measu...
CubeSats are being increasingly specified for demanding Earth observation and astronomical applicati...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83632/1/AIAA-2010-7518-617.pd
A new sensor for measuring low-amplitude magnetic fields that is ideal for small spacecraft is pres...
We present the first in-flight results from a novel miniaturised anisotropic magnetoresistive space...
In the nearly two decades that CubeSats have been in significant use, over 800 have been launched, a...
A magnetometer board intended for CubeSat applications is presented. The board contains four PNI RM3...
For millennia, phenomena of the magnetosphere have intrigued mankind. Studies of the geomagnetic fie...
This report presents the development of a magnetic sensor for use onboard a nano-satellite; it woul...
Motivated by small-scale auroral plasma science, ANDESITE, a 6U CubeSat with eight deployable picosa...
Some space missions require a thorough control of the spacecraft’s magnetic environment. With the ai...
The on board resources, needed to perform the mission tasks, are very limited in nano-satellites. Th...
Researchers from the University of Michigan (UM) and NASA Goddard Spaceflight Center (GSFC) are part...
Space weather research is data-starved and small satellites offer an opportunity to the community. O...
ADCS magnetometers on board of satellites suffer from the disruptive magnetic field produced by the ...
Magnetometer is simple to operate and has fast response. Transducer is rugged and flat and can measu...
CubeSats are being increasingly specified for demanding Earth observation and astronomical applicati...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83632/1/AIAA-2010-7518-617.pd