Accession Number:

ADD005951

Title:

Simplified High Accuracy Guidance System.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s):

Report Date:

1979-03-27

Pagination or Media Count:

5.0

Abstract:

A simplified guidance system for air-to-air missiles where the pilot adjusts his helmet sight to compensate for missile errors and this information is fed to a computer which computes correction data from error information, aircraft position information and missile position information, correction data is then sent via a radio link to the missile control system which changes the flight path accordingly. Author

Subject Categories:

  • Air- and Space-Launched Guided Missiles
  • Fire Control and Bombing Systems
  • Protective Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE