Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets
This paper investigates the use of structured robust techniques for the control design of the aerodynamic descent phase of a reusable rocket. A unified control strategy based on the use of linear-time-invariant structured [Formula: see text] controllers for both attitude and position is proposed and...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2023-05, Vol.46 (5), p.815-837 |
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| container_title | Journal of guidance, control, and dynamics |
| container_volume | 46 |
| creator | Sagliano, Marco Hernández, José A. Macés Farì, Stefano Heidecker, Ansgar Schlotterer, Markus Woicke, Svenja Seelbinder, David Krummen, Sven Dumont, Etienne |
| description | This paper investigates the use of structured robust techniques for the control design of the aerodynamic descent phase of a reusable rocket. A unified control strategy based on the use of linear-time-invariant structured [Formula: see text] controllers for both attitude and position is proposed and verified in both frequency and time domains. The architecture of the controller and the observed performance are discussed. Moreover, the nonlinear behavior of the control strategy is analyzed by looking at both the gain-scheduling law in conditions of plant-controller misalignment through the use of misalignment matrices, and simulation results obtained with a high-fidelity, nonlinear six-degree-of-freedom closed-loop model in perturbed conditions. All the results are based on Cooperative Action Leading to Launcher Innovation in Stage Tossback Operations (CALLISTO), a reusable rocket demonstrator jointly developed by German Aerospace Center (DLR), Japan Aerospace Exploration Agency (JAXA), and National Centre for Space Studies (CNES). |
| doi_str_mv | 10.2514/1.G007077 |
| format | Article |
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Macés ; Farì, Stefano ; Heidecker, Ansgar ; Schlotterer, Markus ; Woicke, Svenja ; Seelbinder, David ; Krummen, Sven ; Dumont, Etienne</creator><creatorcontrib>Sagliano, Marco ; Hernández, José A. Macés ; Farì, Stefano ; Heidecker, Ansgar ; Schlotterer, Markus ; Woicke, Svenja ; Seelbinder, David ; Krummen, Sven ; Dumont, Etienne</creatorcontrib><description>This paper investigates the use of structured robust techniques for the control design of the aerodynamic descent phase of a reusable rocket. A unified control strategy based on the use of linear-time-invariant structured [Formula: see text] controllers for both attitude and position is proposed and verified in both frequency and time domains. The architecture of the controller and the observed performance are discussed. Moreover, the nonlinear behavior of the control strategy is analyzed by looking at both the gain-scheduling law in conditions of plant-controller misalignment through the use of misalignment matrices, and simulation results obtained with a high-fidelity, nonlinear six-degree-of-freedom closed-loop model in perturbed conditions. All the results are based on Cooperative Action Leading to Launcher Innovation in Stage Tossback Operations (CALLISTO), a reusable rocket demonstrator jointly developed by German Aerospace Center (DLR), Japan Aerospace Exploration Agency (JAXA), and National Centre for Space Studies (CNES).</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G007077</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Altitude ; Closed loops ; Controllers ; Gain scheduling ; H-infinity control ; Japanese space program ; Misalignment ; Reusable rocket engines ; Robust control ; Rockets ; Steering ; Velocity</subject><ispartof>Journal of guidance, control, and dynamics, 2023-05, Vol.46 (5), p.815-837</ispartof><rights>Copyright © 2023 by Marco Sagliano, José A. Macés Hernández, Stefano Farì, Ansgar Heidecker, Markus Schlotterer, Svenja Woicke, David Seelbinder, Sven Krummen, Etienne Dumont, and DLR (German Aerospace Center). Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. 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Macés</creatorcontrib><creatorcontrib>Farì, Stefano</creatorcontrib><creatorcontrib>Heidecker, Ansgar</creatorcontrib><creatorcontrib>Schlotterer, Markus</creatorcontrib><creatorcontrib>Woicke, Svenja</creatorcontrib><creatorcontrib>Seelbinder, David</creatorcontrib><creatorcontrib>Krummen, Sven</creatorcontrib><creatorcontrib>Dumont, Etienne</creatorcontrib><title>Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets</title><title>Journal of guidance, control, and dynamics</title><description>This paper investigates the use of structured robust techniques for the control design of the aerodynamic descent phase of a reusable rocket. A unified control strategy based on the use of linear-time-invariant structured [Formula: see text] controllers for both attitude and position is proposed and verified in both frequency and time domains. The architecture of the controller and the observed performance are discussed. Moreover, the nonlinear behavior of the control strategy is analyzed by looking at both the gain-scheduling law in conditions of plant-controller misalignment through the use of misalignment matrices, and simulation results obtained with a high-fidelity, nonlinear six-degree-of-freedom closed-loop model in perturbed conditions. All the results are based on Cooperative Action Leading to Launcher Innovation in Stage Tossback Operations (CALLISTO), a reusable rocket demonstrator jointly developed by German Aerospace Center (DLR), Japan Aerospace Exploration Agency (JAXA), and National Centre for Space Studies (CNES).</description><subject>Altitude</subject><subject>Closed loops</subject><subject>Controllers</subject><subject>Gain scheduling</subject><subject>H-infinity control</subject><subject>Japanese space program</subject><subject>Misalignment</subject><subject>Reusable rocket engines</subject><subject>Robust control</subject><subject>Rockets</subject><subject>Steering</subject><subject>Velocity</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNotkM1qAjEURkNpodZ20TcIdNVF7L3J5MelSKuCULCVLsPMJCljdWKTmYVvr6Krb3P4DhxCnhFGXGLxhqMZgAatb8gApRBMGFPckgFogUzCGO7JQ84bABQK9YD8rNsmNN6xZYx7-tWlvu765B2ds0UbmrbpDnQa2y7FLQ0x0YlP0R3actfUJ9r71LS_NAa68n0uq62nq1j_-S4_krtQbrN_uu6QrD_ev6dztvycLaaTJau51B0T0nAPWCswplSOS6NkQM01Ou2cr3hVcBzLIijnZOlMEZCD5BwQK4FKiSF5ufzuU_zvfe7sJvapPSktN8DBFBLP1OuFqlPMOflg96nZlelgEey5m0V77SaOMsxd6w</recordid><startdate>202305</startdate><enddate>202305</enddate><creator>Sagliano, Marco</creator><creator>Hernández, José A. 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| ispartof | Journal of guidance, control, and dynamics, 2023-05, Vol.46 (5), p.815-837 |
| issn | 0731-5090 1533-3884 |
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| source | Alma/SFX Local Collection |
| subjects | Altitude Closed loops Controllers Gain scheduling H-infinity control Japanese space program Misalignment Reusable rocket engines Robust control Rockets Steering Velocity |
| title | Unified-Loop Structured H-Infinity Control for Aerodynamic Steering of Reusable Rockets |
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