A High-fidelity Performance and Sensitivity Analysis of X-ray Pulsar Navigation in Near-Earth and Cislunar Orbits

被引:0
作者
Winternitz, Luke B. [1 ]
Hassouneh, Munther A. [1 ]
Long, Anne C. [2 ]
Yu, Wayne H. [1 ]
Small, Jeffrey L. [1 ]
Price, Samuel R. [1 ]
Mitchell, Jason W. [3 ]
机构
[1] NASA, Goddard Space Flight Ctr, Code 590, Greenbelt, MD 20771 USA
[2] AI Solut Inc, 4500 Forbes Blvd,Suite 300, Lanham, MD 20706 USA
[3] NASA Headquarters, Washington, DC 20546 USA
来源
PROCEEDINGS OF THE 44TH ANNUAL AMERICAN ASTRONAUTICAL SOCIETY GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE, AAS 2022 | 2024年
关键词
D O I
10.1007/978-3-031-51928-4_37
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Millisecond X-ray pulsars are rapidly rotating neutron stars that emit broadband electromagnetic radiation, including X-rays. These emissions can appear as pulsations to distant observers with long-term stability rivaling laboratory atomic clocks. The concept of using X-ray pulsars for navigation, commonly referred to as XNAV, has a long history in the research literature. Notably, in 2017, NASA's Station Explorer for X-ray Timing and Navigation (SEXTANT) mission, a technology enhancement to the Neutron Star Interior Composition Explorer, made a successful on-orbit demonstration of XNAV on the International Space Station (ISS) in Low-Earth-Orbit. This paper investigates the performance of XNAV in Earth and lunar regimes using a new high-fidelity XNAV analysis tool that builds on tools developed for SEXTANT and uses recent updates to the Goddard Enhanced Onboard Navigation System flight software. Specifically, we study the use of XNAV in an ISS-like orbit for comparison with SEXTANT results, in a highly-inclined geosynchronous orbit, and in an Earth-Moon L1 libration point Near Rectilinear Halo Orbit similar to that proposed for the planned lunar Gateway space station. This paper provides a high-level description of the XNAV analysis tool, baseline predicted performance results, selected sensitivity analyses, and conclusions.
引用
收藏
页码:619 / 637
页数:19
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