The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 20, 2025

Filed:

Sep. 12, 2023
Applicant:

Space Dynamics Laboratory, North Logan, UT (US);

Inventors:

Tyson Smith, Logan, UT (US);

John Akagi, Logan, UT (US);

Greg Droge, Logan, UT (US);

Assignee:

Space Dynamics Laboratory, North Logan, UT (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/24 (2006.01); B64G 1/10 (2006.01); G06F 30/20 (2020.01);
U.S. Cl.
CPC ...
B64G 1/244 (2019.05); B64G 1/1085 (2013.01); G06F 30/20 (2020.01);
Abstract

For maneuvering a spacecraft, a method calculates a virtual point that represents a plurality of spacecraft orbiting in a spacecraft formation. The method further iteratively calculates an inner polytope boundary relative to the virtual point for a given spacecraft of the plurality of spacecraft. In response to determining the inner polytope boundary will be breached, the method maneuvers the given spacecraft to within the inner polytope boundary based on a switching condition, a guidance law, and model predictive control to minimize fuel consumption.


Find Patent Forward Citations

Smith, Tyson. (2025). Maneuvering a spacecraft using an optimized guidance trajectory and model predictive control (U.S. Patent No. 12304664). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12304664

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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