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Structured Robust Control for the Aerodynamic Steering of Reusable Rockets

Marco Sagliano,Stefano Farì, José Macés Hernandéz,Ansgar Heidecker,José Garrido, Matthias Winter,David Seelbinder,Markus Schlotterer,Svenja Woicke,Etienne Dumont

IFAC-PapersOnLine（2022）

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Abstract
This paper investigates the use of structured H∞ control for the aerodynamic descent phase of a reusable rocket. A unified control strategy for attitude and position is proposed and verified. The architecture of the controller, together with the observed performance are discussed. Results are presented for CALLISTO, a reusable rocket demonstrator jointly developed by DLR, JAXA and CNES.
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Key words
Structured H∞,Robust Control,Reusable Rockets,Aeroydnamic Descent,CALLISTO
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