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Design Examples Using μ-Synthesis: Space Shuttle Lateral Axis FCS During Reentry

  • John Doyle
  • Kathryn Lenz
  • Andy Packard
Part of the NATO ASI Series book series (volume 34)

Abstract

This paper studies the application of Structured Singular Values (SSV or μ) for analysis and synthesis of the Space Shuttle lateral axis flight control system (FCS) during reentry. Comparisons are made of the conventional FCS with alternatives based on H -optimal control and μ-synthesis. While this is a fairly standard FCS problem in most respects, the aircraft model is highly uncertain due to the poorly known aerodynamic characteristics (e.g. aero coefficients). The problem as formulated is particularly interesting and challenging because the uncertainty is large and highly structured.

Keywords

Robust Stability Step Response Robust Performance Sensor Noise Nominal Performance 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag Berlin Heidelberg 1987

Authors and Affiliations

  • John Doyle
    • 1
    • 2
  • Kathryn Lenz
    • 1
    • 3
  • Andy Packard
    • 1
    • 4
  1. 1.Systems and Research CenterHoneywell Inc.MinneapolisUSA
  2. 2.California Institute of TechnologyUSA
  3. 3.University of MinnesotaUSA
  4. 4.University of CaliforniaUSA

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