Accession Number:
ADA016932
Title:
Roll-Axis Hydrofluidic Stability Augmentation System Development
Descriptive Note:
Final rept. 29 Mar 1973-30 Sep 1974
Corporate Author:
HONEYWELL INC MINNEAPOLIS MN GOVERNMENT AND AERONAUTICAL PRODUCTS DIV
Personal Author(s):
Report Date:
1975-09-01
Pagination or Media Count:
137.0
Abstract:
The objective of this program was to develop, design, and flight test a roll-axis Hydrofluidic Stability Augmentation System HYSAS for the OH-58A helicopter. The system, when used with a yaw HYSAS, provides increased vehicle damping which improves the handling characteristics. Flight test evaluations were performed with satisfactory results.
Descriptors:
Subject Categories:
- Helicopters