Patent · US Active

Attitude control for a high-altitude balloon

US9254906B1 · kind B1 · utility

24Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 4, 2013
Grant dateFeb 9, 2016
Priority date
Expiry dateJul 26, 2034

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64B1/58
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A high-altitude balloon is provided that may use at least one conductive coil to facilitate attitude control of the balloon. The balloon may include an envelope, a conductive coil, and a control system. The conductive coil may be operatively coupled to the envelope, and the control system may be configured to perform functions. The functions may include determining a measure of rotation with respect to a predetermined orientation of the balloon. The functions may additionally include causing a current to be applied to the conductive coil in a manner such that torque is applied to the envelope that counteracts the measure of rotation and substantially returns the balloon to the predetermined orientation.

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