SBIR/STTR Research Award
Integrated CubeSat ADACS with Reaction Wheels and Star Tracker
Award amount
$949,544Program and phase
SBIR · Phase IIAward year
2013Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- Maryland Aerospace, Inc.
- Proposal award date
- 2013-07-22
- Contract end date
- 2016-09-21
- UEI
- WQ2HKAR812S9
- Solicitation number
- Not reported
- Topic code
- S3.06
Research abstract
The MAI-400SS Space Sextant is a precision attitude determination and control system for CubeSats and Nanosats. The MAI-400SS enables future CubeSat missions with precision fine pointing (0.1deg) and dynamic slewing as will be required for imaging operations of ground targets. A flight control computer, 2 Star Trackers, 3 reaction wheels and 3 electromagnets are incorporated in a 4" x 4" x 3" (3/4U) CubeSat sized module. The system is based on the highly successful MAI-400 miniADACS and extends its performance capability to the 0.1deg range by incorporation of 2 star cameras and attitude determination software. Phase I developed the software algorithms and prototyped the star cameras and electronics. Phase II consists of a development program culminating with a system at TRL 7. The technology is significant because it extends the capability of current low cost Nanosats to tactical imaging and other missions requiring fine pointing and dynamic retargeting, missions hitherto restricted to large and expensive spacecraft. The MAI-400SS will facilitate rapid development of low cost satellites by providing a turnkey system which would be capable of determining and controlling spacecraft attitude automatically; simplifying operations and enabling rapid mission development as envisioned by ORS.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- MAI NimbuSat EO-IR Terrestrial Weather Sensing
- Plug-and-Play Compatibility for CubeSat Attitude Determination and Control Systems
- Integrated CubeSat ADACS with Reaction Wheels and Star Tracker
- MAI-1/2U-ADACS (Attitude Determination and Control System) for CubeSats
- Underwater Mapping and Navigation in GPS-Intermittent Scenarios
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Verified by an exact topic code match. This is not a text-similarity match.
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