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CEAS EuroGNC 2022 |
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Robust Observer-Based Space Launcher Control With Time-Varying Objectives |
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Abstract: This paper presents a novel approach for robust linear time-varying control design for space launchers. It allows the controller to explicitly respect the launcher's highly time-varying dynamics as well as changing control objectives along the ascent trajectory. The latter are readily incorporated via time-varying weighting functions in the mixed sensitivity synthesis. For a more traceable and effective control design a recently proposed weighting scheme is applied, which significantly reduces the controller tuning effort. The synthesis uses a novel observer-based finite horizon linear time-varying (LTV) synthesis approach. It provides a highly structured controller which is easy to implement and facilitates, for example, the incorporation of anti wind-up compensation. The approach is used to design a pitch controller for a small expendable launch vehicle in atmospheric ascent tracking the open-loop guidance reference signal. | ||||||
Keywords: Linear Time-Varying Systems; Observer-Based Control; Space Launcher | ||||||
View PDF CEAS-GNC-2022-065 |
Felix Biertümpfel, Julian Theis, Harald Pfifer: Robust Observer-Based Space Launcher Control With Time-Varying Objectives. Proceedings of the 2022 CEAS EuroGNC conference. Berlin, Germany. May 2022. CEAS-GNC-2022-065. |
BibTeX entry: @Incollection{CEAS-GNC-2022-065, authors = {Biertümpfel, Felix and Theis, Julian and Pfifer, Harald}, title = {Robust Observer-Based Space Launcher Control With Time-Varying Objectives}, booktitle = {Proceedings of the 2022 {CEAS EuroGNC} conference}, address = {Berlin, Germany}, month = may, year = {2022}, note = {CEAS-GNC-2022-065} } |