Structured H∞ control for a launch vehicle

Structured H∞ control for a launch vehicle

This work presents an application of structured H ∞ synthesis, a novel robust controller synthesis technique that takes the benefits of the classic H ∞ synthesis imposing additional restrictions to the controller structure. These restrictions allows the designer to synthesize controllers with a more...

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Hauptverfasser: Knoblauch, M., Saussie, D., Berard, C.
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Aerodynamics
Atmospheric modeling
Complexity theory
Hafnium
Mathematical model
Stability analysis
Vehicles
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creator Knoblauch, M.
Saussie, D.
Berard, C.
description This work presents an application of structured H ∞ synthesis, a novel robust controller synthesis technique that takes the benefits of the classic H ∞ synthesis imposing additional restrictions to the controller structure. These restrictions allows the designer to synthesize controllers with a more understandable structure and help in the optimization process. This technique is applied to the atmospheric ascent phase of a launch vehicle.
doi_str_mv 10.1109/ACC.2012.6315181
format Conference Proceeding
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subjects Aerodynamics
Atmospheric modeling
Complexity theory
Hafnium
Mathematical model
Stability analysis
Vehicles
title Structured H∞ control for a launch vehicle
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