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Title: Compact star-field sensor (SFS)

Abstract

A compact SFS may can be deployed in small space vehicles. The SFS may have a small size, weight, and low power requirements. The hardware, software, catalogs, and calibration algorithm of the SFS provide highly accurate attitude information that can be used for pointing. For instance, accurate attitude determination may be provided that supports pointing of a deployable high gain helical antenna. A full “lost in space” attitude solution, accurate to about an arcminute, may be accomplished in under a minute. The SFS may be fully reprogrammable on orbit, allowing continued algorithm development and deployment after launch.

Inventors:
; ; ; ; ; ; ; ; ; ; ; ;
Issue Date:
Research Org.:
Los Alamos National Laboratory (LANL), Los Alamos, NM (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1824115
Patent Number(s):
11046463
Application Number:
16/043,345
Assignee:
Triad National Security, LLC (Los Alamos, NM)
Patent Classifications (CPCs):
B - PERFORMING OPERATIONS B64 - AIRCRAFT B64G - COSMONAUTICS
G - PHYSICS G01 - MEASURING G01S - RADIO DIRECTION-FINDING
DOE Contract Number:  
AC52-06NA25396
Resource Type:
Patent
Resource Relation:
Patent File Date: 07/24/2018
Country of Publication:
United States
Language:
English
Subject:
79 ASTRONOMY AND ASTROPHYSICS

Citation Formats

Dallmann, Nicholas, Wren, James, Proicou, Michael, Mohr, Hannah, Delapp, Jerry, Katko, Kimberly, Martinez, John, Ortega, Donathan, Seitz, Daniel, Stein, Paul, Tripp, Justin, Warniment, Adam, and Wheat, Jr., Robert. Compact star-field sensor (SFS). United States: N. p., 2021. Web.
Dallmann, Nicholas, Wren, James, Proicou, Michael, Mohr, Hannah, Delapp, Jerry, Katko, Kimberly, Martinez, John, Ortega, Donathan, Seitz, Daniel, Stein, Paul, Tripp, Justin, Warniment, Adam, & Wheat, Jr., Robert. Compact star-field sensor (SFS). United States.
Dallmann, Nicholas, Wren, James, Proicou, Michael, Mohr, Hannah, Delapp, Jerry, Katko, Kimberly, Martinez, John, Ortega, Donathan, Seitz, Daniel, Stein, Paul, Tripp, Justin, Warniment, Adam, and Wheat, Jr., Robert. Tue . "Compact star-field sensor (SFS)". United States. https://www.osti.gov/servlets/purl/1824115.
@article{osti_1824115,
title = {Compact star-field sensor (SFS)},
author = {Dallmann, Nicholas and Wren, James and Proicou, Michael and Mohr, Hannah and Delapp, Jerry and Katko, Kimberly and Martinez, John and Ortega, Donathan and Seitz, Daniel and Stein, Paul and Tripp, Justin and Warniment, Adam and Wheat, Jr., Robert},
abstractNote = {A compact SFS may can be deployed in small space vehicles. The SFS may have a small size, weight, and low power requirements. The hardware, software, catalogs, and calibration algorithm of the SFS provide highly accurate attitude information that can be used for pointing. For instance, accurate attitude determination may be provided that supports pointing of a deployable high gain helical antenna. A full “lost in space” attitude solution, accurate to about an arcminute, may be accomplished in under a minute. The SFS may be fully reprogrammable on orbit, allowing continued algorithm development and deployment after launch.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Jun 29 00:00:00 EDT 2021},
month = {Tue Jun 29 00:00:00 EDT 2021}
}

Works referenced in this record:

Closed loop roll control for momentum biased satellites
patent, October 1980


Sun sensor for orbiting spacecraft
patent, December 1997


Master Control System for Satellite Image Processing
patent-application, October 2019