Patent · US Active

Method, system and apparatus for spacecraft attitude control using B-spline interpolation

US12338003B2 · kind B2 · utility

0Cited by
3References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 4, 2023
Grant dateJun 24, 2025
Priority date
Expiry dateDec 15, 2043

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/48
  • WIPO fieldControl
  • WIPO sectorInstruments

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 spacecraft control system. According to an exemplary embodiment, 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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.