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Accession Number:
ADB031740
Title:
Roll Loop Aeroservoelasticity in the Time Domain.
Corporate Author:
AUBURN UNIV AL DEPT OF AEROSPACE ENGINEERING
Report Date:
1977-09-01
Abstract:
A time domain computer simulation of the roll loop for the YF-16 control system is developed using the Advanced Continuous Simulation Language ACSL. Using stability derivatives developed during frequency domain studies, the time domain simulation results in excellent agreement, although slightly unconservative, with experienced in-flight instabilities. Author
Descriptive Note:
Final rept. 12 Oct 76-30 Sep 77,
Pages:
0101
Contract Number:
F08635-77-C-0007
File Size:
0.00MB
