CubeSat development for CANYVAL-X mission

Jae Pil Park; Sang Young Park; Young Bum Song; Guk Nam Kim; Kwangwon Lee; Hyungjik Jay Oh; Jin Chul Yim; Eun Ji Lee; Soon Hong Hwang; Sung Woo Kim; Kyung Yun Choi; Dong Shin Lee; Sang Hoon Kwon; Min Sik Kim; Seung Won Yeo; Tae Hyun Kim; Seung Hee Lee; Kang Been Lee; Joong Won Seo; Won Hyuk Cho; Jungpyo Lee; Jung Hyun Park; Yong Woo Kim; Seok Ju Kang; Jiyoon Hwang; Soo Hwi Lee; Jin Ho Yang; Sungmin Jin

CubeSat development for CANYVAL-X mission

Jae Pil Park, Sang Young Park, Young Bum Song, Guk Nam Kim, Kwangwon Lee, Hyungjik Jay Oh, Jin Chul Yim, Eun Ji Lee, Soon Hong Hwang, Sung Woo Kim, Kyung Yun Choi, Dong Shin Lee, Sang Hoon Kwon, Min Sik Kim, Seung Won Yeo, Tae Hyun Kim, Seung Hee Lee, Kang Been Lee, Joong Won Seo, Won Hyuk ChoJungpyo Lee, Jung Hyun Park, Yong Woo Kim, Seok Ju Kang, Jiyoon Hwang, Soo Hwi Lee, Jin Ho Yang, Sungmin Jin

Institute of Earth·Atmosphere·Astronomy(BK21+)

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

CANYVAL-X mission is developed for demonstrating a virtual telescope alignment system. The main objective of this mission is to build an inertial alignment of a virtual telescope with respect to the Sun during a few minutes by using two CubeSats, Tom(2U) and Jerry(1U). Inertial alignment is to maintain relative position and relative attitude of the two satellites with respect to the target object. For achieving the inertial alignment, a vision alignment system, relative position control with thruster, relative orbit determination with inter-satellite link system and satellite separation system need to be developed. This study presents an overview of the mission concept and configuration systems of Tom and Jerry.

Original language	English
Title of host publication	14th International Conference on Space Operations
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624104268
Publication status	Published - 2016
Event	14th International Conference on Space Operations, 2016 - Daejeon, Korea, Republic of Duration: 2016 May 16 → 2016 May 20

Publication series

Name	14th International Conference on Space Operations, 2016

Other

Other	14th International Conference on Space Operations, 2016
Country	Korea, Republic of
City	Daejeon
Period	16/5/16 → 16/5/20

Bibliographical note

Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

Fingerprint Dive into the research topics of 'CubeSat development for CANYVAL-X mission'. Together they form a unique fingerprint.

Cite this

Park, J. P., Park, S. Y., Song, Y. B., Kim, G. N., Lee, K., Oh, H. J., Yim, J. C., Lee, E. J., Hwang, S. H., Kim, S. W., Choi, K. Y., Lee, D. S., Kwon, S. H., Kim, M. S., Yeo, S. W., Kim, T. H., Lee, S. H., Lee, K. B., Seo, J. W., ... Jin, S. (2016). CubeSat development for CANYVAL-X mission. In 14th International Conference on Space Operations (14th International Conference on Space Operations, 2016). American Institute of Aeronautics and Astronautics Inc, AIAA.

Park, Jae Pil ; Park, Sang Young ; Song, Young Bum ; Kim, Guk Nam ; Lee, Kwangwon ; Oh, Hyungjik Jay ; Yim, Jin Chul ; Lee, Eun Ji ; Hwang, Soon Hong ; Kim, Sung Woo ; Choi, Kyung Yun ; Lee, Dong Shin ; Kwon, Sang Hoon ; Kim, Min Sik ; Yeo, Seung Won ; Kim, Tae Hyun ; Lee, Seung Hee ; Lee, Kang Been ; Seo, Joong Won ; Cho, Won Hyuk ; Lee, Jungpyo ; Park, Jung Hyun ; Kim, Yong Woo ; Kang, Seok Ju ; Hwang, Jiyoon ; Lee, Soo Hwi ; Yang, Jin Ho ; Jin, Sungmin. / CubeSat development for CANYVAL-X mission. 14th International Conference on Space Operations. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (14th International Conference on Space Operations, 2016).

@inproceedings{489fb0be000f47cb897bb307eb2354b2,

title = "CubeSat development for CANYVAL-X mission",

abstract = "CANYVAL-X mission is developed for demonstrating a virtual telescope alignment system. The main objective of this mission is to build an inertial alignment of a virtual telescope with respect to the Sun during a few minutes by using two CubeSats, Tom(2U) and Jerry(1U). Inertial alignment is to maintain relative position and relative attitude of the two satellites with respect to the target object. For achieving the inertial alignment, a vision alignment system, relative position control with thruster, relative orbit determination with inter-satellite link system and satellite separation system need to be developed. This study presents an overview of the mission concept and configuration systems of Tom and Jerry.",

author = "Park, {Jae Pil} and Park, {Sang Young} and Song, {Young Bum} and Kim, {Guk Nam} and Kwangwon Lee and Oh, {Hyungjik Jay} and Yim, {Jin Chul} and Lee, {Eun Ji} and Hwang, {Soon Hong} and Kim, {Sung Woo} and Choi, {Kyung Yun} and Lee, {Dong Shin} and Kwon, {Sang Hoon} and Kim, {Min Sik} and Yeo, {Seung Won} and Kim, {Tae Hyun} and Lee, {Seung Hee} and Lee, {Kang Been} and Seo, {Joong Won} and Cho, {Won Hyuk} and Jungpyo Lee and Park, {Jung Hyun} and Kim, {Yong Woo} and Kang, {Seok Ju} and Jiyoon Hwang and Lee, {Soo Hwi} and Yang, {Jin Ho} and Sungmin Jin",

note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 14th International Conference on Space Operations, 2016 ; Conference date: 16-05-2016 Through 20-05-2016",

year = "2016",

language = "English",

isbn = "9781624104268",

series = "14th International Conference on Space Operations, 2016",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "14th International Conference on Space Operations",

}

Park, JP, Park, SY, Song, YB, Kim, GN, Lee, K, Oh, HJ, Yim, JC, Lee, EJ, Hwang, SH, Kim, SW, Choi, KY, Lee, DS, Kwon, SH, Kim, MS, Yeo, SW, Kim, TH, Lee, SH, Lee, KB, Seo, JW, Cho, WH, Lee, J, Park, JH, Kim, YW, Kang, SJ, Hwang, J, Lee, SH, Yang, JH & Jin, S 2016, CubeSat development for CANYVAL-X mission. in 14th International Conference on Space Operations. 14th International Conference on Space Operations, 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, 14th International Conference on Space Operations, 2016, Daejeon, Korea, Republic of, 16/5/16.

CubeSat development for CANYVAL-X mission. / Park, Jae Pil; Park, Sang Young; Song, Young Bum; Kim, Guk Nam; Lee, Kwangwon; Oh, Hyungjik Jay; Yim, Jin Chul; Lee, Eun Ji; Hwang, Soon Hong; Kim, Sung Woo; Choi, Kyung Yun; Lee, Dong Shin; Kwon, Sang Hoon; Kim, Min Sik; Yeo, Seung Won; Kim, Tae Hyun; Lee, Seung Hee; Lee, Kang Been; Seo, Joong Won; Cho, Won Hyuk; Lee, Jungpyo; Park, Jung Hyun; Kim, Yong Woo; Kang, Seok Ju; Hwang, Jiyoon; Lee, Soo Hwi; Yang, Jin Ho; Jin, Sungmin.

14th International Conference on Space Operations. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (14th International Conference on Space Operations, 2016).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

TY - GEN

T1 - CubeSat development for CANYVAL-X mission

AU - Park, Jae Pil

AU - Park, Sang Young

AU - Song, Young Bum

AU - Kim, Guk Nam

AU - Lee, Kwangwon

AU - Oh, Hyungjik Jay

AU - Yim, Jin Chul

AU - Lee, Eun Ji

AU - Hwang, Soon Hong

AU - Kim, Sung Woo

AU - Choi, Kyung Yun

AU - Lee, Dong Shin

AU - Kwon, Sang Hoon

AU - Kim, Min Sik

AU - Yeo, Seung Won

AU - Kim, Tae Hyun

AU - Lee, Seung Hee

AU - Lee, Kang Been

AU - Seo, Joong Won

AU - Cho, Won Hyuk

AU - Lee, Jungpyo

AU - Park, Jung Hyun

AU - Kim, Yong Woo

AU - Kang, Seok Ju

AU - Hwang, Jiyoon

AU - Lee, Soo Hwi

AU - Yang, Jin Ho

AU - Jin, Sungmin

PY - 2016

Y1 - 2016

N2 - CANYVAL-X mission is developed for demonstrating a virtual telescope alignment system. The main objective of this mission is to build an inertial alignment of a virtual telescope with respect to the Sun during a few minutes by using two CubeSats, Tom(2U) and Jerry(1U). Inertial alignment is to maintain relative position and relative attitude of the two satellites with respect to the target object. For achieving the inertial alignment, a vision alignment system, relative position control with thruster, relative orbit determination with inter-satellite link system and satellite separation system need to be developed. This study presents an overview of the mission concept and configuration systems of Tom and Jerry.

AB - CANYVAL-X mission is developed for demonstrating a virtual telescope alignment system. The main objective of this mission is to build an inertial alignment of a virtual telescope with respect to the Sun during a few minutes by using two CubeSats, Tom(2U) and Jerry(1U). Inertial alignment is to maintain relative position and relative attitude of the two satellites with respect to the target object. For achieving the inertial alignment, a vision alignment system, relative position control with thruster, relative orbit determination with inter-satellite link system and satellite separation system need to be developed. This study presents an overview of the mission concept and configuration systems of Tom and Jerry.

UR - http://www.scopus.com/inward/record.url?scp=84979982407&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84979982407&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84979982407

SN - 9781624104268

T3 - 14th International Conference on Space Operations, 2016

BT - 14th International Conference on Space Operations

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 14th International Conference on Space Operations, 2016

Y2 - 16 May 2016 through 20 May 2016

ER -

CubeSat development for CANYVAL-X mission

Abstract

Publication series

Other

Bibliographical note

All Science Journal Classification (ASJC) codes

Other files and links

Cite this