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Payload Flight Number:
2009-12
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Institution:
Texas A&M
University
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Payload Title:
Second Look Intelligent Calibration Cameras System (SLICC)
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Student Leader:
Ron Denton
Computer Science
Spacecraft Technology
Center
Texas A&M
University - MS 3118
College Station, TX 77843-3118
Denton.r@tamu.edu
Telephone:
979-845-8768
Fax:
979-847-8857
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Faculty Advisor:
Dr. Thomas J. Talley P.E.
Spacecraft
Technology Institute
Texas A&M
University - MS 3118
College Station, TX 77843-3118
talley@tamu.edu
Telephone:
979-845-8768
Cell:
903-244-6996
Fax:
979-847-8857
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Payload class:
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Large
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Payload ID
Number:
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12
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Mass:
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Current:
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Serial Downlink:
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Analog Downlink:
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Serial Commands:
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Discrete
Commands:
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Payload Specification & Integration Plan
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Due: 6/1/2009
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Delivered:
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Payload Integration Certification
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Scheduled: 8/2/09
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Actual:
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Flight Operation Plan
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Due:
8/2/09
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Delivered:
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Final Flight / Science Report
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Due: 12/18/2009
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Delivered:
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Abstract:
The Second Look Intelligent Calibration
Cameras System (SLICC) is designed to compare ccd and cmos imagers in a near
space environment for use in attitude determination of spacecraft. The camera systems will be integrated
and tested by a student team from the Space Engineering Institute of Texas
A&M University led by a graduate student, Ron Denton, who developed the
initial single camera system which flew in 2008. The development of smaller and lighter
ccd and cmos imagers for use as “star trackers” on spacecraft is continuing.
There are many differences in the systems and side by side comparisons of
these technologies in “near space” would be helpful in understanding the
practical strengths and weaknesses of each technology. We propose to supply
a package which will implement two cameras pointed at dark sky which is
clear of the balloon’s envelope and the horizon with control computers and
telemetry (thus needing to be positioned with a relatively unobstructed view
upward and outward from the top of the HASP package). Each camera would take
images using experimental software which can perform image analysis and
optimization and conversion of star field information to Quaternions for use
in attitude estimation. An Az/El
mount will allow the cameras to be aimed away from the sun and toward parts
of the sky containing sparse star populations to maximally test various
“star tracker” attitude determination techniques. Bi-directional telemetry
will allow switching software applications and image processing parameter
results to be conducted by the ground team.
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