Lunar Orbit Design of a Satellite Swarm for Radio Astronomy

Sung-Hoon Mok; Jian Guo; Eberhard Gill; Raj Thilak Rajan

doi:10.1109/AERO47225.2020.9172468

Lunar Orbit Design of a Satellite Swarm for Radio Astronomy

Sung-Hoon Mok, Jian Guo, Eberhard Gill, Raj Thilak Rajan

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

3 Citations (Scopus)

42 Downloads (Pure)

Abstract

Employing a satellite swarm for radio astronomy has been continuously addressed in the Orbiting Low Frequency ARray (OLFAR) project. A 100 km diameter of aperture array constructed by distributed satellites will be able to provide sky maps of better than 1 arc-minute spatial resolution at 10 MHz. However, an orbit design strategy for the swarm satellites that ensures safe intersatellite distances and relative orbit stability has not yet been developed. In this paper, a new method for OLFAR orbit design is proposed. A deterministic solution is presented based on three algebraic constraints derived here, which represent three orbit design requirements: collision avoidance, maximum baseline rate, and uvw-space coverage. In addition, an idea for observation planning over the mission lifetime is presented.

Original language	English
Title of host publication	2020 IEEE Aerospace Conference
Publisher	IEEE
Pages	1-9
Number of pages	9
ISBN (Electronic)	978-1-7281-2734-7
ISBN (Print)	978-1-7281-2735-4
DOIs	https://doi.org/10.1109/AERO47225.2020.9172468
Publication status	Published - 2020
Event	2020 IEEE Aerospace Conference, AERO 2020 - Big Sky, United States Duration: 7 Mar 2020 → 14 Mar 2020

Conference

Conference	2020 IEEE Aerospace Conference, AERO 2020
Country/Territory	United States
City	Big Sky
Period	7/03/20 → 14/03/20

Access to Document

10.1109/AERO47225.2020.9172468

09172468Final published version, 932 KB

Cite this

@inproceedings{dde0dfd5c9064192a3bb56fcd71f5fc3,

title = "Lunar Orbit Design of a Satellite Swarm for Radio Astronomy",

abstract = "Employing a satellite swarm for radio astronomy has been continuously addressed in the Orbiting Low Frequency ARray (OLFAR) project. A 100 km diameter of aperture array constructed by distributed satellites will be able to provide sky maps of better than 1 arc-minute spatial resolution at 10 MHz. However, an orbit design strategy for the swarm satellites that ensures safe intersatellite distances and relative orbit stability has not yet been developed. In this paper, a new method for OLFAR orbit design is proposed. A deterministic solution is presented based on three algebraic constraints derived here, which represent three orbit design requirements: collision avoidance, maximum baseline rate, and uvw-space coverage. In addition, an idea for observation planning over the mission lifetime is presented.",

author = "Sung-Hoon Mok and Jian Guo and Eberhard Gill and Rajan, {Raj Thilak}",

year = "2020",

doi = "10.1109/AERO47225.2020.9172468",

language = "English",

isbn = "978-1-7281-2735-4",

pages = "1--9",

booktitle = "2020 IEEE Aerospace Conference",

publisher = "IEEE",

address = "United States",

note = "2020 IEEE Aerospace Conference, AERO 2020 ; Conference date: 07-03-2020 Through 14-03-2020",

}

TY - GEN

T1 - Lunar Orbit Design of a Satellite Swarm for Radio Astronomy

AU - Mok, Sung-Hoon

AU - Guo, Jian

AU - Gill, Eberhard

AU - Rajan, Raj Thilak

PY - 2020

Y1 - 2020

N2 - Employing a satellite swarm for radio astronomy has been continuously addressed in the Orbiting Low Frequency ARray (OLFAR) project. A 100 km diameter of aperture array constructed by distributed satellites will be able to provide sky maps of better than 1 arc-minute spatial resolution at 10 MHz. However, an orbit design strategy for the swarm satellites that ensures safe intersatellite distances and relative orbit stability has not yet been developed. In this paper, a new method for OLFAR orbit design is proposed. A deterministic solution is presented based on three algebraic constraints derived here, which represent three orbit design requirements: collision avoidance, maximum baseline rate, and uvw-space coverage. In addition, an idea for observation planning over the mission lifetime is presented.

AB - Employing a satellite swarm for radio astronomy has been continuously addressed in the Orbiting Low Frequency ARray (OLFAR) project. A 100 km diameter of aperture array constructed by distributed satellites will be able to provide sky maps of better than 1 arc-minute spatial resolution at 10 MHz. However, an orbit design strategy for the swarm satellites that ensures safe intersatellite distances and relative orbit stability has not yet been developed. In this paper, a new method for OLFAR orbit design is proposed. A deterministic solution is presented based on three algebraic constraints derived here, which represent three orbit design requirements: collision avoidance, maximum baseline rate, and uvw-space coverage. In addition, an idea for observation planning over the mission lifetime is presented.

UR - http://www.scopus.com/inward/record.url?scp=85092601319&partnerID=8YFLogxK

U2 - 10.1109/AERO47225.2020.9172468

DO - 10.1109/AERO47225.2020.9172468

M3 - Conference contribution

AN - SCOPUS:85092601319

SN - 978-1-7281-2735-4

SP - 1

EP - 9

BT - 2020 IEEE Aerospace Conference

PB - IEEE

T2 - 2020 IEEE Aerospace Conference, AERO 2020

Y2 - 7 March 2020 through 14 March 2020

ER -

Lunar Orbit Design of a Satellite Swarm for Radio Astronomy

Abstract

Conference

Access to Document

Other files and links

Fingerprint

Cite this