Patent · US Active

Satellite control system

US10734092B2 · kind B2 · utility

0Cited by
15References
6Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 18, 2019
Grant dateAug 4, 2020
Priority date
Expiry dateJun 18, 2039

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG12B7/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A vehicle, a satellite control system, and a method for controlling the same are provided. The satellite control system, for example, may include, but is not limited to, a control moment gyroscope having a gimbal, at least one gimbal angle sensor configured to determine an angle of the gimbal, each gimbal angle sensor having an output circuit configured to output the determined angle, a signal conditioner circuit having substantially identical circuit topology as the output circuit, and a common mode error compensation circuit electrically coupled to the signal conditioner, the common mode error compensation circuit configured to determine common mode error in the gimbal angle sensor based upon a voltage output from the signal conditioner circuit and to output a signal to compensate for the common mode error.

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