Optimization-Based Phase-Constrained x-Axis Crossing Control for Station-Keeping on Libration Point Orbits

Author(s)
Shimane, Yuri
Weiss, Avishai
Advisor(s)
Editor(s)
Associated Organization(s)
Organizational Unit
Daniel Guggenheim School of Aerospace Engineering
The Daniel Guggenheim School of Aeronautics was established in 1931, with a name change in 1962 to the School of Aerospace Engineering
Series
Supplementary to:
Abstract
Libration Point Orbits (LPO) play a central role in lunar exploration of the twenty first century. Long-term operations of both crewed and robotic assets on LPOs necessitate propellant-efficient and reliable station-keeping schemes. Recent developments highlight the importance of station-keeping schemes that not only maintain the geometric orbital regime but also avoid leading or lagging along the orbit as a result of a drifting phase. In this work, an optimization-based station-keeping algorithm for colinear LPO based on the x-axis crossing control, an event-based targeting scheme for impulsive maneuver design, is conceived. The optimization problem is cast as a sequential second-order cone program and incorporates an explicit constraint on the perilune pass epoch to ensure the steered trajectory follows the reference baseline without deviating in phase. The resulting formulation has easily interpretable tuning parameters that may be obtained directly from mission requirements. The algorithm is demonstrated through Monte-Carlo simulations on Gateway’s Near Rectilinear Halo Orbit (NRHO) in the high-fidelity ephemeris model with realistic error models.
Sponsor
Date
2025
Extent
Resource Type
Text
Resource Subtype
Rights Statement
Unless otherwise noted, all materials are protected under U.S. Copyright Law and all rights are reserved