Guidance command generation and nonlinear dynamic inversion control for reusable launch vehicles

Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are currently investigated by the DLR research projects Akira and X-tras. In particular, the winged Liquid Fly-back Booster concept Lfbb based on an LOX/LH2 propellant combination for vertical takeoff and ver...

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Veröffentlicht in:	Acta astronautica 2020-09, Vol.174, p.334-346
Hauptverfasser:	Acquatella B, Paul, Briese, Lâle Evrim, Schnepper, Klaus
Format:	Artikel
Sprache:	eng
Schlagworte:	Architecture Control stability Controllability Delta wings Dynamic inversion Expendable launch vehicles Guidance Inversion Kerosene Liquid oxygen Nonlinear control Nonlinear dynamics Preliminary designs Research projects Reusable launch vehicles Reusable space launchers Rockets Spacecraft Tracking Trajectory optimization Vehicles Vertical landing Vertical takeoff
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