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.
|Title of host publication||SpaceOps 2016 Conference|
|Publisher||American Institute of Aeronautics and Astronautics Inc, AIAA|
|Publication status||Published - 2016|
|Event||14th International Conference on Space Operations, SpaceOps 2016 - Daejeon, Korea, Republic of|
Duration: 2016 May 16 → 2016 May 20
|Name||SpaceOps 2016 Conference|
|Other||14th International Conference on Space Operations, SpaceOps 2016|
|Country||Korea, Republic of|
|Period||16/5/16 → 16/5/20|
Bibliographical notePublisher Copyright:
© 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering
- Acoustics and Ultrasonics