DEBRIS AVOIDANCE AND PHASE CHANGE MANEUVERS IN NEAR RECTILINEAR HALO ORBITS

被引：0

作者：

Davis, Diane C. ^{[1
]}

Zimovan-Spreen, Emily M. ^{[2
]}

Scheuerle, Stephen T. ^{[3
]}

Howell, Kathleen C. ^{[3
]}

机构：

[1] AI Solut Inc, 2224 Bay Area Blvd, Houston, TX 77058 USA

[2] NASA, Johnson Space Ctr, Flight Mech & Trajectory Design Branch, Houston, TX USA

[3] Purdue Univ, Sch Aeronaut & Astronaut, Armstrong Hall Engn,701 W Stadium Ave, W Lafayette, IN 47907 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_35

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Over the course of its lifetime, Gateway may execute excursions from its baseline NRHO that include short-lead maneuvers to avoid other spacecraft or debris objects or long-lead rephasing within the NRHO to support rendezvous or other mission objectives. The dynamical characteristics of the NRHO are distinct from those of low Earth and low lunar orbits due to the simultaneous gravitational influences of the Earth and Moon. Thus, new approaches for executing debris avoidance maneuvers (DAMs) and rephasing maneuvers are necessary. The current investigation proposes strategies for designing low-cost DAMs with short-lead planning time as well as rephasing maneuvers with many months of advance notice.

引用

页码：585 / 600

页数：16

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