Accession Number:

ADA003634

Title:

A Universal Flight Director Computer.

Descriptive Note:

Final rept.

Corporate Author:

AERONAUTICAL SYSTEMS DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-08-01

Pagination or Media Count:

60.0

Abstract:

A technique is proposed which will make the flight director computer performance independent of aircraft dynamics, wind or aircraft position relative to the navigation beam. The control law proposed will compensate for all such variables with an error correcting mechanism. This technique results in a computer that is universal in its application.

Subject Categories:

  • Computer Programming and Software

Distribution Statement:

APPROVED FOR PUBLIC RELEASE