A high-order target phase approach for the station-keeping of periodic orbits

Author:

Fu Xiaoyu,Baresi Nicola,Armellin Roberto

Abstract

AbstractA novel high-order target phase approach (TPhA) for the station-keeping of periodic orbits is proposed in this work. The key elements of the TPhA method, the phase-angle Poincare map and high-order maneuver map, are constructed using differential algebra (DA) techniques to determine station-keeping epochs and calculate correction maneuvers. A stochastic optimization framework tailored for the TPhA-based station-keeping process is leveraged to search for fuel-optimal and error-robust TPhA parameters. Quasi-satellite orbits (QSOs) around Phobos are investigated to demonstrate the efficacy of TPhA in mutli-fidelity dynamical models. Monte Carlo simulations demonstrated that the baseline QSO of JAXA’s Martian Moons eXploration (MMX) mission could be maintained with a monthly maneuver budget of approximately 1 m/s.

Publisher

Springer Science and Business Media LLC

Reference29 articles.

1. Guzzetti, D., Zimovan, E. M., Howell, K. C., Davis, D. C. Stationkeeping analysis for spacecraft in lunar near rectilinear halo orbits. In: Proceedings of the 27th AAS/AIAA Space Flight Mechanics Meeting, San Antonio, TX, USA, 2017, 160: 3199–3218.

2. Qi, Y., de Ruiter, A. Station-keeping strategy for real translunar libration point orbits using continuous thrust. Aerospace Science and Technology, 2019, 94: 105376.

3. LaFarge, N. B., Miller, D., Howell, K. C., Linares, R. Autonomous closed-loop guidance using reinforcement learning in a low-thrust, multi-body dynamical environment. Acta Astronautica, 2021, 186: 1–23.

4. Zhang, R. K., Wang, Y., Shi, Y., Zhang, C., Zhang, H. Performance analysis of impulsive station-keeping strategies for cis-lunar orbits with the ephemeris model. Acta Astronautica, 2022, 198: 152–160.

5. Folta, D., Pavlak, T., Howell, K., Woodard, M., Woodfork, D. Stationkeeping of Lissajous trajectories in the Earth–Moon system with applications to ARTEMIS. In: Proceedings of the 20th AAS/AIAA Space Flight Mechanics Meeting, San Diego, CA, USA, 2010: AAS 10-113.

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