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Accession Number:
ADA010492
Title:
A Technique for Mapping Aircraft Stability Boundaries
Corporate Author:
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
Report Date:
1975-05-01
Abstract:
This study presents a method for determining the effect that variations in design parameters may have on the transient response characteristics of a system of differential equations. The effects of single design parameter variations are described using a modified root locus technique. Simultaneous variations of two or three parameters are described using stability region maps.
Descriptive Note:
Final rept. Jul 1973-Dec 1974
Supplementary Note:
Prepared in cooperation with ARO, Inc., Tullahoma, Tenn. Rept. no. ARO-PWT-TR-75-14.
Pages:
0056
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
1.74MB
