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 Jan 1 |
| 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 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science
Cite this
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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 - 2016/1/1
Y1 - 2016/1/1
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
ER -