Automatic Solar and Celestial Navigation on the Moon and Mars

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$100,000.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
NNX10CD46P
Award Id:
95406
Agency Tracking Number:
094712
Solicitation Year:
n/a
Solicitation Topic Code:
O4
Solicitation Number:
n/a
Small Business Information
800 West Ninth Avenue, Denver, CO, 80204
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
084022110
Principal Investigator:
Richard Speck
Principal Investigator
(303) 595-9696
rpspeck@hotmail.com
Business Contact:
Richard Speck
Business Official
(303) 595-9696
rpspeck@hotmail.com
Research Institute:
n/a
Abstract
Micro-Space proposes to develop a low mass, automated form of the classic navigator's bubble sextant, with no moving parts, for rapid localization and reliable navigation on the Moon and Mars. Day, night, near side and far side lunar operations will all be handled. Exploration of the Moon (or Mars) without navigation aids comparable to those now common on Earth is a daunting, and generally unacceptable concept. Since neither body has a significant magnetic field, even a compass is useless. Creating and sustaining a GPS type satellite constellation will not occur soon. But the self contained, automated system Micro-Space proposes is an excellent substitute. It can be installed on top of an astronaut's helmet, or atop a vehicle, in extended EVA. With exploration extended into terrain where a vehicle is likely to become immobilized, but access by a walking human is practical, vast areas of currently unknown territory can be examined at very close range. But an hour's trek into convoluted terrain can leave the trekker seriously disoriented, and subject to human course decisions which could prove fatal. The helmet mount system will provide continuous EVA crew localization for emergency walk back to a safe haven, even if that path crosses unexplored territory. Fixed asset or notable planetary feature localization will also be straightforward at any point in the EVA. The proposed optical navigation system uses production, solid state camera modules for Solar, Earth Shine, and Celestial sight readings, all with an accurate artificial horizon. But the accuracy required is produced by Micro-Space proprietary "Sub Pixel" processing techniques. Lunar localization accuracy will exceed

* information listed above is at the time of submission.

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