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CEAS EuroGNC 2026 |
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Lunar Lander Variable-Mass Dynamics Modeling Considering Propellant Sloshing |
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| Abstract: Precision landings on the lunar surface are essential for accessing scientifically valuable sites and enabling future lunar base operations. Achieving such accuracy demands high-fidelity representations of the spacecraft dynamics during early GNC development phases. This work addresses two major challenges in modeling lunar lander dynamics: 1) the accurate capturing of variable-mass dynamics due to rapid propellant consumption, and 2) the characterization of sloshing-induced perturbations, which are strongly dependent on the fill level and the lander's acceleration. Expanding upon a rigid body dynamical model, in this paper we derive a set of nonlinear equations of motion that incorporates both variable-mass effects and sloshing dynamics using a pendulum-based approximation parameterized for spherical tanks. The formulation is modular and scalable, allowing a straightforward integration of multiple tanks and propulsion systems. The model's validity is demonstrated through a simplified lunar lander scenario showing very close alignment with published data on sloshing mode characteristics. | ||||||||
| Keywords: GNC Design; Lunar Lander; Variable Mass; Propellant Sloshing; Equations of Motion | ||||||||
| Carl-Johann Winkler, Paul Acquatella, Francesco Capolupo, Harald Pfifer: Lunar Lander Variable-Mass Dynamics Modeling Considering Propellant Sloshing. Proceedings of the 2026 CEAS EuroGNC conference. Madrid, Spain. May 2026. doi: 10.82124/CEAS-GNC-2026-041. |
| BibTeX entry (UTF-8): @Incollection{CEAS-GNC-2026-041, author = {Winkler, Carl-Johann and Acquatella, Paul and Capolupo, Francesco and Pfifer, Harald}, title = {Lunar Lander Variable-Mass Dynamics Modeling Considering Propellant Sloshing}, booktitle = {Proceedings of the 2026 {CEAS EuroGNC} conference}, address = {Madrid, Spain}, month = may, year = {2026}, doi = {10.82124/CEAS-GNC-2026-041} } |