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Attitude Determination and Control Systems for
Mini, Micro and Nanosatellites
Maryland Aerospace Inc.
Products
Presenting our growing line of miniature ADACS products and systems. Originally developed under DARPA sponsorship, our portfolio now includes products for 3 axis zero momentum, magnetic momentum bias, Earth sensors and Sun Sensors. Custom development available, please inquire at: discover@miniadacs.com

Note: Quantity pricing & academic discounts are available! Please request a quote.
MAI-100
Complete standalone attitude determination and control system for microsatellites. Includes 3 axis reaction / momentum wheels, electromagnets, magnetometer, sun sensor, ADACS computer. Designed for mechanical compatibility with CubeSat kits.
MAI-101
Wheels only version of the MAI-100. Three 1.1 mNms reaction / momentum wheels in a 3" hermetically sealed package. No ADACS computer, electromagnets or sensors.
MAI-200
A larger version of the MAI-100 for minisats up to 20 kg. Achieves 10x the momentum capacity of the MAI-100 with high speed motors. Includes 3 axis reaction / momentum wheels, electromagnets, magnetometer, sun sensor, ADACS computer. Same weight and size as the MAI-100.
MAI-201
Wheels only version of the MAI-200. Three 11 mNms reaction / momentum wheels in a 3" hermetically sealed package. No ADACS computer, electromagnets or sensors. Same weight and size.
Static Earth Sensor
Earth limb sensor for day/night attitude determination. Two are required for roll and pitch sensing.
Dynamic Simulator
Facilitates real time hardware-in-the-loop simulation of miniADACS products. Runs on PC and interfaces with MAI-100 / 200 / 300. Run different mission scenarios and verify ADACS performance. A necessity for ground test and control law and software validation.
Copyright © Maryland Aerospace, Inc. All rights reserved.
MAI-300
Miniature single-axis reaction wheel.
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MAI-400 A La Carte- NEW!
The newest ADACS for CubeSat applications at only 1/2U in size. Features the most technologically advanced reacion wheel system by MAI. Integrates optional Earth Horizon Sensor cameras for complete attitude determination.
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