- Main Features
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High accuracy in eclipse
Earth Observation missions
Spin stabilised three axis control
Simple magnetic control
Acquiring stabilisation and orbital information
TDS-1 IN 2014
Selected by a number of other CubeSat clients
Single PC104 form factor
Low power
I2C and UART interfaces
Can be populated to mission requirements
Dimensions: 96 x 96 x 15mm
Mass: <2000g
Power: 1.8W
NSS CubeSat ACS board
A CubeSat Attitude Control System (ACS) measures orbit position, absolute attitude, spacecraft rates and can also control the orientation of the satellite through either magnetic actuation or wheel based solutions. The NewSpace ACS board is a single PC104 board (15mm height) that physically integrates three high accuracy sun sensors, a magnetometer, MEMS gyros, a stellar gyro and two magnetorquer rods. Additionally, external interfaces allow for a further three sun sensors, the Z-axis magnetorquer as well as momentum or reaction wheels.
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