Plug-and-Play Compatibility for CubeSat Attitude Determination and Control Systems

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$124,716.00
Program:
SBIR
Contract:
NNX12CD74P
Solitcitation Year:
2011
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2012
Phase:
Phase I
Agency Tracking Number:
114447
Solicitation Topic Code:
O1.03
Small Business Information
Maryland Aerospace, Inc
2138 Priest Bridge Court, Suite 3, Crofton, MD, -
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
125532908
Principal Investigator
 Steve Fujikawa
 Principal Investigator
 (410) 451-2505
 sfujikawa@imicro.biz
Business Contact
 Steve Fujikawa
Title: Business Official
Phone: (410) 451-2505
Email: sfujikawa@imicro.biz
Research Institution
 Stub
Abstract
The development of Plug-and-play Compatibility for CubeSat Attitude Determination and Control Systems (ADACS) is proposed. Existing Maryland Aerospace (MAI) ADACS technologies are well-capable of autonomously providing complete attitude determination and control to satellites weighing up to 20kg. It is essential for these ADACS technologies to be fully compliant with a Plug-and-Play standard that allows them to integrate seamlessly into rapid spacecraft development. One solution for Plug-and-Play is the Space Plug-and-play Architecture (SPA) bus developed by the Air Force Research Laboratory (AFRL), which is currently being adopted by many spacecraft developers for its low-cost, low-power, and simple design. A program for development of the electronics and firmware is outlined to create SPA compatibility technologies for CubeSat and NanoSat ADACS. This technology is significant because not only does it extend the capability of current low cost spacecraft to tactical imaging, space environment monitoring, and other missions requiring precision fine pointing, it provides a tremendous amount of flexibility in spacecraft mission design. Future NASA spacecraft development will no longer have to expend time and energy to develop an attitude solution.

* information listed above is at the time of submission.

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