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CANYVAL-X Mission Development Using CubeSats

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Space Operations: Contributions from the Global Community

Abstract

Current space telescopes have a single structure, and consequently, their focal length cannot be increased sufficiently. Sometimes, this problem may prevent the improvement of the resolution of the telescope. To solve this problem, the concept of virtual telescope has been proposed. A virtual telescope consists of two spacecraft: one has a lens system and the other has a detector system. By using formation flying, the two spacecraft can be simplified as a virtual telescope system. Then, their relative orbit distance can serve as a baseline for the virtual telescope system [1, 2]. The most important issue in a virtual telescope is to perform inertial alignment with respect to a celestial object and to maintain it in space. Inertial alignment means that the relative position and relative attitude of the two spacecraft are simultaneously aligned with a target.

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References

  1. Shah, N., Calhoun P.C., Dennis, B.R., Krizmanic, J.F., Shih, A.Y., Skinner G.K.: The virtual telescope demonstration mission. In: 5th International Conference on Spacecraft Formation Flying Missions and Technologies, Munich, Germany, May 29–31, 2013

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  2. Park, S.-Y., Calhoun, P.C., Shah, N., Williams, T.W.: Orbit design and control of technology validation mission for refractive space telescope in formation flying. In: AIAA Guidance, Navigation, and Control Conference, SciTech 2014, National Harbor, Maryland, AIAA-2014-0451, January 13–17, 2014

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  3. Dennis, B.R., Skinner, G.K., Li, M.J., Shih, A.Y.: Very high-resolution solar X-ray imaging using diffractive optics. Solar Phys. 279(2), 573–588 (2012)

    Article  Google Scholar 

  4. Haque, S.E., George, T., Keidar, M., Agasid, E.F., Gazulla, O.T., Perez, A.D., Trinh, G.T., Uribe, E.A.: Micro cathode arc thruster phonesat experiment for small satellites. In: The 33rd International Electric Propulsion Conference, The George Washington University, Washington, D.C., October 6–10, 2013

    Google Scholar 

  5. van Bolhuis, M.F., Overlack, A.E., Bonnema, A.R.: Environment Levels ISILaunch09 Auxiliary Payloads, 1.2 version. Innovative Space Logistics, Delft (2015)

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Acknowledgments

This study was supported by the National Research Foundation of Korea through the Space Core Technology Development Program funded by the Ministry of Science, ICT, and Future Planning (2013M1A3A3A02042448).

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Correspondence to Sang-Young Park .

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Park, JP. et al. (2017). CANYVAL-X Mission Development Using CubeSats. In: Cruzen, C., Schmidhuber, M., Lee, Y., Kim, B. (eds) Space Operations: Contributions from the Global Community. Springer, Cham. https://doi.org/10.1007/978-3-319-51941-8_30

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  • DOI: https://doi.org/10.1007/978-3-319-51941-8_30

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