Orbital debris has become an inevitable problem for the future space exploration, and spacecraft is suggested to remove orbital debris. To fulfill this mission, you need to know target's attitude motion when installing a mitigation-related device. To support, we developed a simulator of orbit, attitude, and light curve to see how an object behaves. This paper presents a process to simulate virtual rocket body's observation in LEO assuming an existing telescope in Kyushu University, and to estimate the triaxial ratio, the spin axis, and the shape model. The real observation is supposed to be held in the near future.
|ジャーナル||Advances in the Astronautical Sciences|
|出版物ステータス||出版済み - 1 1 2013|
|イベント||23rd AAS/AIAA Space Flight Mechanics Meeting, Spaceflight Mechanics 2013 - Kauai, HI, 米国|
継続期間: 2 10 2013 → 2 14 2013
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science