Method, System and Apparatus for Spacecraft Attitude Control Using B-Spline Interpolation

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Authors
Karpenko, Mark
Ross, Isaac M.
Levitas, Joshua
Cristi, Roberto
Subjects
Advisors
Date of Issue
2025-06-24
Date
Publisher
The Government of the United States of America, as represented by the Secretary of the Navy, Washington, DC (US)
Language
Abstract
A method, apparatus and system for controlling an attitude of a spacecraft, the spacecraft including an attitude control system operatively associated with a ground-based spaceĀ­ craft control system. According to an exemplary embodiĀ­ ment, the spacecraft attitude control system uses a B-spline interpolator for commanding the spacecraft. The methods and systems disclosed herein can be implemented in, for example, executable machine code and/or integrated circuit hardware.
Type
Patent
Description
Series/Report No
Department
Identifiers
US 12,338,003 B2
NPS Report Number
Sponsors
Funder
Format
56 p.
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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