Numerical Analysis of Relative Orbit Control Strategy for CANYVAL-X Mission |
Lee, Youngro
(Department of Astronomy, Yonsei University)
Park, Sang-Young (Department of Astronomy, Yonsei University) Park, Jae-Pil (Department of Astronomy, Yonsei University) Song, Youngbum (Department of Astronomy, Yonsei University) |
1 | Lee K, Oh HJ, Kang SJ, Sim JS, Park JP, et al., Design of attitude determination and control system for cube satellite in CANYVAL-X mission, Proceeding of the 2014 The Korean Space Science Society, Jeju-do, Republic of Korea, 29-31 Oct 2014. |
2 | Lee Y, Park SY, Park JP, Song Y, Numerical analysis of the relative orbit control strategy of the CANYVAL-X mission, Master's Thesis, Yonsei University (2018). |
3 | Lemmer K, Propulsion for cubesats, Acta Astronaut. 134, 231-243 (2017). https://doi.org/10.1016/j.actaastro.2017.01.048 DOI |
4 | Liu H, Li J, Hexi B, Sliding mode control for low-thrust Earthorbiting spacecraft formation maneuvering, Aerosp. Sci. Technol. 10, 636-643 (2006). https://doi.org/10.1016/j.ast.2006.04.008 DOI |
5 | Orr NG, Eyer JK, Larouche BP, Zee RE, Precision formation flight: the CanX-4 and CanX-5 dual nanosatellite mission, in 21th Annual AIAA/USU Conference on Samll Satellites, Logan, UT, 13-16 Jan 2007. |
6 | Park JP, Park SY, Song YB, Kim GN, Lee K, et al., CANYVAL-X mission development using CubeSats, In Space Operations: Contributions from the Global Community, eds. Cruzen1 C, Schmidhuber M, Lee YH, Kim B (Springer, Cham, Switzerland, 2017), 681-691. |
7 | Park JP, Park SY, Song YB, Kim GN, Lee K, et al., System development for CANYVAL-X (cubesat astronomy NASA and Yonsei by using virtual telescope ALignmenteXperiment) mission, Proceeding of The Korean Society for Aeronautical and Space Sciences Spring Conference, Gangwon-do, Republic of Korea, 20-22 Apr 2016. |
8 | Schaub H. Relative orbit geometry through classical orbit element differences, J. Guide Control Dyn. 27, 839-848, (2004). https://doi.org/10.2514/1.12595 DOI |
9 | Tummala AR, Dutta A, An overview of cube-satellite propulsion technologies and trends, Aerospace, 4, 58 (2017). https://doi.org/10.3390/aerospace4040058 DOI |
10 | Leonard CL, Hollister WM, Bergmann EV, Orbital formationkeeping with differential drag, J. Guide Control Dyn. 12, 108-113 (1989). https://doi.org/10.2514/3.20374 DOI |
11 | Kvell U, Puusepp M, Kaminski F, Past JE, Palme K, et al., Nanosatellite orbit control using MEMS cold gas thrusters, Proc. East Acad. Sci. 63, 279-285 (2014). https://doi.org/10.3176/proc.2014.2S.09 DOI |
12 | Bonin G, Roth N, Armitage S, Newman J, Risi B, et al., CanX-4 and CanX-5 precision formation flight: mission accomplished!, in 29th Annual AIAA/USU Conference on Samll Satellites, Logan, UT, 8 Aug 2015. |
13 | Cho HC, Park SY, Analytic solution for fuel-optimal reconfiguration in relative motion, J. Optimiz. Theory App, 141, 495-512 (2009). https://doi.org/10.1007/s10957-008-9482-3 DOI |
14 | Foster C, Mason J, Vittaldev V, Leung L, Beukelaers V, et al., Differential drag control scheme for large constellation of planet satellites and on-orbit results, Proceeding of the 9th International Workshop on Satellite Constellations and Formation Flying, University of Colorado, Boulder, CO, 19-21 Jun 2017. |
15 | Gill E, Sundaramoorthy P, Bouwmeester J, Zandbergen B, Reinhard R, Formation flying within a constellation of nanosatellites: the QB50 mission, Acta. Astronaut. 82, 110-117 (2013). https://doi.org/10.1016/j.actaastro.2012.04.029 DOI |
16 | Han S, Choi Y, Cho DH, Choi WS, Gong HC, et al., Analysis of cubesat development status in Korea, J. Korean Soc. Aeronaut. Space Sci. 45, 975-988 (2017). https://doi.org/10.5139/JKSAS.2017.45.11.975 |
17 | Keidar M. Micro-Cathode Arc Thruster for small satellite propulsion, In 53rd AIAA Aerospace Sciences Meeting, Kissimmee, FL, 5-9 Jan 2015. https://doi.org/10.2514/6.2015-0938 |
18 | Kumar BS, Ng A, Yoshihara K, Ruiter AD, Differential drag as a means of spacecraft formation control, IEEE Trans. Aerosp. Electron. Sys. 47, 1125-1135 (2007). https://doi.org/10.1109/TAES.2011.5751247 DOI |