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.

Sagliano, M., Fari, S., Hernandez, J.M., Heidecker, A., Garrido, J., Winter, M., et al. (2022). Structured Robust Control for the Aerodynamic Steering of Reusable Rockets. Elsevier B.V. [10.1016/j.ifacol.2022.09.319].

Structured Robust Control for the Aerodynamic Steering of Reusable Rockets

Sagliano M.;
2022

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.
2022
IFAC-PapersOnLine
31
36
Sagliano, M., Fari, S., Hernandez, J.M., Heidecker, A., Garrido, J., Winter, M., et al. (2022). Structured Robust Control for the Aerodynamic Steering of Reusable Rockets. Elsevier B.V. [10.1016/j.ifacol.2022.09.319].
Sagliano, M.; Fari, S.; Hernandez, J. M.; Heidecker, A.; Garrido, J.; Winter, M.; Seelbinder, D.; Schlotterer, M.; Woicke, S.; Dumont, E.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11585/1041816
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