Accession Number:

AD0854666

Title:

In-Flight Investigation of the Effect on PIO of Control System Nonlinearities, Pitch Acceleration and Normal Acceleration Bobweights.

Descriptive Note:

Final rept.,

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

• Newell, Fred D.
• Wasserman, Richard

Report Date:

1969-05-01

Pagination or Media Count:

128.0

Abstract:

Descriptors:

• *HUMAN FACTORS ENGINEERING)
• (*FLIGHT CONTROL SYSTEMS
• ELEVATORS
• PILOTS
• OSCILLATION
• CONTROL STICKS
• HANDLING
• HYSTERESIS
• PITCH(MOTION)
• ACCELERATION
• FLIGHT TESTING
• STABILITY

Subject Categories:

• Aircraft
• Human Factors Engineering and Man Machine Systems

Distribution Statement:

APPROVED FOR PUBLIC RELEASE