Evolution of the out-of-plane amplitude for quasi-periodic trajectories in the Earth–Moon system |
| |
| Institution: | 1. Department of Aerospace Engineering, San José State University, 1 Washington Square, San José, CA 95192-0179, United States;2. School of Aeronautics and Astronautics, Purdue University, 701 W. Stadium Ave., West Lafayette, IN 47907-2045, United States;1. Advanced Space Concepts Laboratory, Department of Mechanical and Aerospace Engineering, University of Strathclyde, 75 Montrose Street, Glasgow G1 1XJ, Scotland, United Kingdom;2. Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft, The Netherlands |
| |
| Abstract: | The out-of-plane amplitude along quasi-periodic trajectories in the Earth–Moon system is highly sensitive to perturbations in position and/or velocity as underscored recently by the ARTEMIS spacecraft. Controlling the evolution of the out-of-plane amplitude is non-trivial, but can be critical to satisfying mission requirements. The sensitivity of the out-of-plane amplitude evolution to perturbations due to lunar eccentricity, solar gravity, and solar radiation pressure is explored and a strategy for designing low-cost deterministic maneuvers to control the amplitude history is also examined. The method is sufficiently general and is applied to the L1 quasi-periodic orbit that serves as a baseline for the ARTEMIS P2 trajectory. |
| |
| Keywords: | |
| 本文献已被 ScienceDirect 等数据库收录！ |
|
