Loading…

Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft

The main objective of this research effort is to achieve an accuracy level for the SimSat star tracker system comparable to what is reported in current literature by various star tracker manufacturers and researchers. Previous work has provided a spherical star dome that needs to be fully populated...

Full description

Saved in:
Bibliographic Details
Main Author: Grunwald, Warren C
Format: Report
Language:English
Subjects:
Online Access:Request full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by
cites
container_end_page
container_issue
container_start_page
container_title
container_volume
creator Grunwald, Warren C
description The main objective of this research effort is to achieve an accuracy level for the SimSat star tracker system comparable to what is reported in current literature by various star tracker manufacturers and researchers. Previous work has provided a spherical star dome that needs to be fully populated with light sources. Programmable organic light emitting diode (OLED) panels were chosen to populate the dome to allow high contrast ratios without backlighting and increase the number of star combinations able to be represented. Noise equivalent angles less than five arcseconds (1 delta ) are achieved about the boresight axis and less than half an arcsecond around the other axes. Absolute accuracy near the center of the star dome is tested to be less than 0.04 degree about each axis. Two different approaches to inertially cataloging the star eld are also investigated, externally referencing each panels coordinates using a coordinate measurement arm and utilizing the camera's known position to catalog the panel's location. The full population of the SimSat star dome and reprogrammable capability of the panels allows many future research endeavors related to star pattern recognition and attitude determination to be undertaken. The original document contains color images.
format report
fullrecord <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA600298</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA600298</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA6002983</originalsourceid><addsrcrecordid>eNqFi7sKwkAQAK-xEPUPLPYHAkFBtEyMYilewDKsl71weA_ZWwv_3ivsraaYmbm6d5TdFCFZQLhymhhDwIcn0IIMPaN5ElctZhrhRpaYoinyk4UC2MRl0y68PUoJ9AsNGUYrSzWz6DOtflyo9fnUHy_VKM4MWVwkGZqu2dX15rDf_tFfjyI2Bw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft</title><source>DTIC Technical Reports</source><creator>Grunwald, Warren C</creator><creatorcontrib>Grunwald, Warren C ; AIR FORCE INSTITUTE OF TECHNOLOGY WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT</creatorcontrib><description>The main objective of this research effort is to achieve an accuracy level for the SimSat star tracker system comparable to what is reported in current literature by various star tracker manufacturers and researchers. Previous work has provided a spherical star dome that needs to be fully populated with light sources. Programmable organic light emitting diode (OLED) panels were chosen to populate the dome to allow high contrast ratios without backlighting and increase the number of star combinations able to be represented. Noise equivalent angles less than five arcseconds (1 delta ) are achieved about the boresight axis and less than half an arcsecond around the other axes. Absolute accuracy near the center of the star dome is tested to be less than 0.04 degree about each axis. Two different approaches to inertially cataloging the star eld are also investigated, externally referencing each panels coordinates using a coordinate measurement arm and utilizing the camera's known position to catalog the panel's location. The full population of the SimSat star dome and reprogrammable capability of the panels allows many future research endeavors related to star pattern recognition and attitude determination to be undertaken. The original document contains color images.</description><language>eng</language><subject>ATTITUDE(INCLINATION) ; COMPUTER PROGRAMMING ; Computer Programming and Software ; DYNAMICS ; SIMULATORS ; SPACECRAFT ; STAR TRACKERS ; Unmanned Spacecraft</subject><creationdate>2014</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA600298$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Grunwald, Warren C</creatorcontrib><creatorcontrib>AIR FORCE INSTITUTE OF TECHNOLOGY WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT</creatorcontrib><title>Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft</title><description>The main objective of this research effort is to achieve an accuracy level for the SimSat star tracker system comparable to what is reported in current literature by various star tracker manufacturers and researchers. Previous work has provided a spherical star dome that needs to be fully populated with light sources. Programmable organic light emitting diode (OLED) panels were chosen to populate the dome to allow high contrast ratios without backlighting and increase the number of star combinations able to be represented. Noise equivalent angles less than five arcseconds (1 delta ) are achieved about the boresight axis and less than half an arcsecond around the other axes. Absolute accuracy near the center of the star dome is tested to be less than 0.04 degree about each axis. Two different approaches to inertially cataloging the star eld are also investigated, externally referencing each panels coordinates using a coordinate measurement arm and utilizing the camera's known position to catalog the panel's location. The full population of the SimSat star dome and reprogrammable capability of the panels allows many future research endeavors related to star pattern recognition and attitude determination to be undertaken. The original document contains color images.</description><subject>ATTITUDE(INCLINATION)</subject><subject>COMPUTER PROGRAMMING</subject><subject>Computer Programming and Software</subject><subject>DYNAMICS</subject><subject>SIMULATORS</subject><subject>SPACECRAFT</subject><subject>STAR TRACKERS</subject><subject>Unmanned Spacecraft</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>2014</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFi7sKwkAQAK-xEPUPLPYHAkFBtEyMYilewDKsl71weA_ZWwv_3ivsraaYmbm6d5TdFCFZQLhymhhDwIcn0IIMPaN5ElctZhrhRpaYoinyk4UC2MRl0y68PUoJ9AsNGUYrSzWz6DOtflyo9fnUHy_VKM4MWVwkGZqu2dX15rDf_tFfjyI2Bw</recordid><startdate>20140327</startdate><enddate>20140327</enddate><creator>Grunwald, Warren C</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>20140327</creationdate><title>Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft</title><author>Grunwald, Warren C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA6002983</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>2014</creationdate><topic>ATTITUDE(INCLINATION)</topic><topic>COMPUTER PROGRAMMING</topic><topic>Computer Programming and Software</topic><topic>DYNAMICS</topic><topic>SIMULATORS</topic><topic>SPACECRAFT</topic><topic>STAR TRACKERS</topic><topic>Unmanned Spacecraft</topic><toplevel>online_resources</toplevel><creatorcontrib>Grunwald, Warren C</creatorcontrib><creatorcontrib>AIR FORCE INSTITUTE OF TECHNOLOGY WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Grunwald, Warren C</au><aucorp>AIR FORCE INSTITUTE OF TECHNOLOGY WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft</btitle><date>2014-03-27</date><risdate>2014</risdate><abstract>The main objective of this research effort is to achieve an accuracy level for the SimSat star tracker system comparable to what is reported in current literature by various star tracker manufacturers and researchers. Previous work has provided a spherical star dome that needs to be fully populated with light sources. Programmable organic light emitting diode (OLED) panels were chosen to populate the dome to allow high contrast ratios without backlighting and increase the number of star combinations able to be represented. Noise equivalent angles less than five arcseconds (1 delta ) are achieved about the boresight axis and less than half an arcsecond around the other axes. Absolute accuracy near the center of the star dome is tested to be less than 0.04 degree about each axis. Two different approaches to inertially cataloging the star eld are also investigated, externally referencing each panels coordinates using a coordinate measurement arm and utilizing the camera's known position to catalog the panel's location. The full population of the SimSat star dome and reprogrammable capability of the panels allows many future research endeavors related to star pattern recognition and attitude determination to be undertaken. The original document contains color images.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_dtic_stinet_ADA600298
source DTIC Technical Reports
subjects ATTITUDE(INCLINATION)
COMPUTER PROGRAMMING
Computer Programming and Software
DYNAMICS
SIMULATORS
SPACECRAFT
STAR TRACKERS
Unmanned Spacecraft
title Design of a Programmable Star Tracker-Based Reference System for a Simulated Spacecraft
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-31T01%3A13%3A41IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=Design%20of%20a%20Programmable%20Star%20Tracker-Based%20Reference%20System%20for%20a%20Simulated%20Spacecraft&rft.au=Grunwald,%20Warren%20C&rft.aucorp=AIR%20FORCE%20INSTITUTE%20OF%20TECHNOLOGY%20WRIGHT-PATTERSON%20AFB%20OH%20GRADUATE%20SCHOOL%20OF%20ENGINEERING%20AND%20MANAGEMENT&rft.date=2014-03-27&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EADA600298%3C/dtic_1RU%3E%3Cgrp_id%3Ecdi_FETCH-dtic_stinet_ADA6002983%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true