Accession Number:

ADA046363

Title:

Glide Path Augmentation with Inertial Flight Path Angle.

Descriptive Note:

Final rept. Jan 72-Dec 74,

Corporate Author:

BENDIX CORP TETERBORO N J FLIGHT SYSTEMS DIV

Personal Author(s):

Report Date:

1974-12-01

Pagination or Media Count:

36.0

Abstract:

A two segment approach configuration using inertially derived flight path angle to damp the glide path and upper segment approach paths is developed in the text. System performance in both head and tail winds is evaluated. Stability analysis is also presented on root locus plots for the capture and track modes. Author

Subject Categories:

  • Air Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE