Accession Number:
ADA000894
Title:
Three-Axis Fluidic/Electronic Automatic Flight Control System Flight Test Report
Descriptive Note:
Final rept. 1 Jun 1973-25 Jan 1974
Corporate Author:
UNITED TECHNOLOGIES CORP STRATFORD CT SIKORSKY AIRCRAFT DIV
Personal Author(s):
Report Date:
1974-08-01
Pagination or Media Count:
126.0
Abstract:
This report covers the flight test of a three-axis Hydrofluidic Stability Augmentation System HYSAS coupled with a completely independent parallel attitude and heading hold for a CH-54B helicopter. The design goal was to evaluate the performance of the CH-54B Automatic Flight Control System AFCS with the electronic SAS replaced with a fluidic SAS and to establish the technical base for a fluidic inner loop and electronic outer loop control system.
Descriptors:
Subject Categories:
- Helicopters
- Fluidics and Fluerics