Patent · US Expired

Optical attitude reference

US4072281A · kind A · utility

18Cited by
4References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 27, 1976
Grant dateFeb 7, 1978
Priority date
Expiry dateDec 27, 1996

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF41G7/26
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

The optical attitude reference system provides missile attitude reference ing an optical beam in lieu of conventional gyroscopes. In the missile control systems autopilot, the system uses the properties of polarized light to determine missile roll angle relative to the beam transmitter reference axes at the launch site.

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