HASP 2009 HASP 2008 HASP 2007 HASP 2006

Payload Flight Number:

2009-12

Institution:

Texas A&M University

Payload Title:

Second Look Intelligent Calibration Cameras System (SLICC)

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

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

 

Payload class:

Large

Payload ID Number:

12

Mass:

 

Current:

 

Serial Downlink:

 

Analog Downlink:

 

Serial Commands:

 

Discrete Commands:

 

 

 

Payload Specification & Integration Plan

Due: 6/1/2009

Delivered:

Payload Integration Certification

Scheduled: 8/2/09

Actual:

Flight Operation Plan

Due:  8/2/09

Delivered:

Final Flight / Science Report

Due: 12/18/2009

Delivered:

 

 

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.

 

Payload Application:

TAMU_HASP_2009
Payload Integration Plan:

Payload Specification and Integration Plan
Science Report:

Final Briefing:

Summary Status:

Original

Summary Date:

January 6, 2009

 
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