Accession Number:

ADA128331

Title:

Development of the MICROSAS Longitudinal Flight Control System for the Augmentor Wing Aircraft (Mise au Point du Systeme de Controle en Tangage MICROSAS pour l'avion a Aile a Volets Trompes).

Descriptive Note:

Aeronautical note,

Corporate Author:

NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)

Personal Author(s):

Report Date:

1983-02-01

Pagination or Media Count:

38.0

Abstract:

A digital longitudinal stability augmentation system was designed and installed in the Augmentor Wing Research Aircraft by the Flight Research Laboratory of the National Aeronautical Establishment. This system partially replaced the computer-controlled control and display system called STOLAND owned by NASA Ames Research Center that was removed from the aircraft prior to its return to Canada. The computer system is described and the software flow charts are illustrated. Brief comments on the performance of the system during the flight test program are included.

Subject Categories:

  • Aerodynamics
  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE