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 : MAY 1969

Pagination or Media Count : 128

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 & Man Machine System

Distribution Statement : APPROVED FOR PUBLIC RELEASE