Roll Loop Aeroservoelasticity in the Time Domain.
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1977
- Accession Number
- ADB031740
Entities
People
- Malcolm A. Cutchins
Organizations
- Auburn University