Small Business Innovation Research/Small Business Tech Transfer
Ultra-Miniaturized Star Tracker for Small Satellite Attitude Control, Phase I
Project Introduction
Creare and Virginia Polytechnic Institute and State University propose to design, develop, test, and deliver an ultra compact star tracker specifically intended for small satellites such as the CubeSat platform. Our design is based on proprietary "folded optics" technology previously developed by our partner for use in military and commercial optical applications that require a compact footprint and high performance. The folded optics design is superior to conventional refractive optics in miniature star trackers because (1) the compact footprint is achieved without sacrificing accuracy; (2) the light-gathering aperture is much greater, leading to better sensitivity; (3) the aperture geometry makes the shielding baffles smaller; and (4) the imaging sensor can be shielded efficiently from cosmic radiation. During the Phase I project, we will demonstrate the feasibility of our innovation by finalizing the design, performing analysis to determine the optimal design parameters, and testing a benchtop prototype to verify the design models. In Phase II, we will fabricate the optimized design, test the prototype in the laboratory and in the field, and deliver the prototype to NASA.
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Anticipated Benefits
Many NASA science missions are exploring the use of pico- and nano-satellites as alternatives to expensive, large satellites. In order to enable many mission profiles, these satellites need attitude determination sensors. Our star tracker will enable highly precise attitude determination (e.g., 10 arc seconds or better) in a package that is significantly smaller, has much lower mass, and uses less power than any alternative star trackers on the market. As the market for and uses of small and nano satellites increases, the demand for our star tracker will increase to enable missions that are not possible with today's technology. Both the military and commercial ventures are looking to small satellites to provide a cost effective space mission platform. However, the majority of missions still require high attitude accuracy. There is therefore a need for high-accuracy star tracker technology. Furthermore, the military is looking at star trackers for high-altitude unmanned aerial vehicle (UAV) attitude determination. These will typically need to provide arc-second accuracy in a small form factor with low power demands, which makes our proposed miniaturized star tracker ideally suited.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Creare LLC | Lead Organization | Industry | Hanover, New Hampshire |
Goddard Space Flight Center
(GSFC)
|
Supporting Organization | NASA Center | Greenbelt, Maryland |
| Virginia Polytechnic Institute and State University (VA Tech) | Supporting Organization | Academia | Blacksburg, Virginia |
Primary U.S. Work Locations
-
Maryland
-
New Hampshire
-
Virginia
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Creare LLC
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: May 2013
End: May 2014
Technology Maturity (TRL)
| Start: | 3 |
| Current: | 5 |
| Estimated End: | 5 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX17 Guidance, Navigation, and Control (GN&C)
- TX17.2 Navigation Technologies
- TX17.2.3 Navigation Sensors
Target Destination
Earth
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