Accession Number:

ADA339046

Title:

Investigation of Feel System and Control Sensitivity Characteristics Influencing P-I-O of Unmaneuverable Aircraft

Descriptive Note:

Final rept.

Corporate Author:

TSENTRAL'NYI AERO-GIDRODINAMICHE'SKII INST MOSCOW (RUSSIA)

Report Date:

1995-01-01

Pagination or Media Count:

78.0

Abstract:

This report results from a contract tasking TsAGI, Central Aerohydrodynamic Institute as follows Investigate the pilot-induced-oscillation PIO tendency depending upon control sensitivity characteristics, damping of lever loading, lever mass and loading gradient at different flight regimes and dynamic performance using flight simulators.

Subject Categories:

  • Flight Control and Instrumentation

Distribution Statement:

APPROVED FOR PUBLIC RELEASE