SHORT-TIME STABILITY IN LINEAR TIME-VARYING SYSTEMS

Abstract

The concept of short-time stability finds application in missile and satellite systems where operating times are often of finite duration. Short-time stability assures, in a finite time interval, that all inputs bounded by a prescribed constant Greek epsilon result in outputs bounded by a second prescribed constant. The study of short-time stability is divided into two categories: undriven systems and driven systems. Undriven systems are represented by a set of differential equations. Sufficient conditions for short-time stability are given in terms of the coefficients. Driven systems are represented by their impulse response. A necessary and sufficient condition for short-time stability in driven systems is given directly in terms of impulse response. Sufficient conditions for short-time stability in feedback systems, in terms of the open loop impulse response are also included. In addition the concept of shorttime C-equivalence, essentially a structural stability concept, is introduced. Necessary and sufficient conditions for two systems to be short-time C-equivalent are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 09, 1961
Accession Number
AD0258397

Entities

People

  • Peter Dorato

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Closed Loop Systems
  • Coefficients
  • Differential Equations
  • Equations
  • Feedback
  • Intervals
  • Mathematics
  • Time Intervals

Fields of Study

  • Mathematics

Readers

  • Control Systems Engineering.

Technology Areas

  • Space