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):

Report Date:

1969-05-01

Pagination or Media Count:

128.0

Abstract:

Subject Categories:

  • Aircraft
  • Human Factors Engineering and Man Machine Systems

Distribution Statement:

APPROVED FOR PUBLIC RELEASE