The rise of CubeSats has highlighted the need for mission analysis that integrates uncertainties inside the optimization phase. This work incorporates uncertainties in initial conditions, maneuvers, and navigation into a stochastic trajectory optimization process. It uses a novel implementation of the unscented transformation, avoiding sigma points resampling by employing a continuous propagation map. The problem is formulated as a nonlinear programming problem and applied to weak stability boundary trajectories, with the LUMIO mission as a case study. The method yields more fuel-efficient and robust trajectories compared to deterministic optimization. Monte Carlo analyses validate the effectiveness and accuracy of the approach.

Optimization of Weak Stability Boundary Transfers Under Uncertainty: the LUMIO Mission Case

Martinelli, A.;Buonagura, C.;Giordano, C.;Topputo, F.
2025-01-01

Abstract

The rise of CubeSats has highlighted the need for mission analysis that integrates uncertainties inside the optimization phase. This work incorporates uncertainties in initial conditions, maneuvers, and navigation into a stochastic trajectory optimization process. It uses a novel implementation of the unscented transformation, avoiding sigma points resampling by employing a continuous propagation map. The problem is formulated as a nonlinear programming problem and applied to weak stability boundary trajectories, with the LUMIO mission as a case study. The method yields more fuel-efficient and robust trajectories compared to deterministic optimization. Monte Carlo analyses validate the effectiveness and accuracy of the approach.
2025
35th AAS/AIAA Space Flight Mechanics Meeting
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1284812
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