Accession Number:

AD0880252

Title:

An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 2. Appendices 1 through 5

Descriptive Note:

Final rept.

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

• Neal, T. P.
• Smith, Rogers E.

Report Date:

1970-12-01

Pagination or Media Count:

175.0

Abstract:

Contents Pilot comments, bode plots, time histories for each configuration Analysis of data using equivalent dynamics Complete C time histories Longitudinal transfer functions Details of simulation mechanization and data reduction techniques.

Descriptors:

• *FIGHTER AIRCRAFT
• *FLIGHT CONTROL SYSTEMS
• SIMULATION
• FLIGHT TESTING
• STABILITY
• PITCH(MOTION)
• STATISTICAL DATA
• AERIAL WARFARE
• STANDARDS

Subject Categories:

• Attack and Fighter Aircraft
• Training Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE