NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Stability analysis of large space structure control systems with delayed inputLarge space structural systems, due to their inherent flexibility and low mass to area ratio, are represented by large dimensional mathematical models. For implementation of the control laws for such systems a finite amount of time is required to evaluate the control signals; and this time delay may cause instability in the closed loop control system that was previously designed without taking the input delay into consideration. The stability analysis of a simple harmonic oscillator representing the equation of a single mode as a function of delay time is treated analytically and verified numerically. The effect of inherent damping on the delay is also analyzed. The control problem with delayed input is also formulated in the discrete time domain.
Document ID
19890004095
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reddy, A. S. S. R.
(Howard Univ. Washington, DC, United States)
Bainum, Peter M.
(Howard Univ. Washington, DC, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Publication Information
Publication: NASA, Langley Research Center, Proceedings of the 4th Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: VPI and SU/AIAA Symposium on Dynamics and Control of Large Structures
Location: Washington, DC
Country: Unted States
Start Date: January 1, 1988
Accession Number
89N13466
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available