2018 IEEE/ION Position, Location and Navigation Symposium (PLANS) 2018
DOI: 10.1109/plans.2018.8373517
|View full text |Cite
|
Sign up to set email alerts
|

Navigating to small-bodies using small satellites

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2019
2019
2023
2023

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(3 citation statements)
references
References 7 publications
0
3
0
Order By: Relevance
“…Then the cameras obtain information and data from the above satellites, thus avoiding space collisions and conducting autonomous sensing and detection of in-orbit threats for avoidance or countermeasures. In regard to extraterrestrial planet detection, there are many intelligent SWaP 3 IRCs developed for rover systems applying for exploration of Mars, the Moon, etc., which usually undertake tasks such as surface environment detection and analysis of planets [11,55,56].…”
Section: Applications 261 Military and Scientific Fieldmentioning
confidence: 99%
“…Then the cameras obtain information and data from the above satellites, thus avoiding space collisions and conducting autonomous sensing and detection of in-orbit threats for avoidance or countermeasures. In regard to extraterrestrial planet detection, there are many intelligent SWaP 3 IRCs developed for rover systems applying for exploration of Mars, the Moon, etc., which usually undertake tasks such as surface environment detection and analysis of planets [11,55,56].…”
Section: Applications 261 Military and Scientific Fieldmentioning
confidence: 99%
“…However, only a few small-spacecraft mission concepts can be found in literature leveraging autonomous deep-space navigation-although none of which has yet been funded for implementation-namely: the SRMSAT-2 86-kg small-spacecraft study to orbit the Moon [26,27], the BIRDY 3U CubeSat study on a transfer trajectory to Mars [28], the DustCube 3U CubeSat mission proposal to the Didymos binary asteroid system [29], the LOGIC-X 12U CubeSat mission proposal in close proximity to an asteroid [30], and the LUMIO 12U CubeSat study around the Earth-Moon second Lagrange point [31].…”
Section: Introductionmentioning
confidence: 99%
“…The growing interest in the development of highly capable nanosatellites for a wide range of scientific missions [1][2][3][4][5] demands a substantial increase of the traditionally low success rate of this kind of miniaturized platforms, which were originally conceived for educational or technological demonstration purposes. Among the causes for their low success rate, the limited ground verification process, especially at sub-system and system levels, is a relevant one, often originating due to schedule and budget constraints.…”
Section: Introductionmentioning
confidence: 99%