Preliminary simulation for light curves of rocket body in LEO

Hideaki Hinagawa, Toshiya Hanada

研究成果: ジャーナルへの寄稿Conference article

抄録

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.

元の言語英語
ページ(範囲)1755-1767
ページ数13
ジャーナルAdvances in the Astronautical Sciences
148
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 20132 14 2013

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low Earth orbits
Rockets
rockets
debris
Debris
light curve
simulator
mitigation
spacecraft
orbitals
space exploration
curves
Telescopes
simulators
installing
simulation
Spacecraft
Orbits
Simulators
telescopes

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

これを引用

Preliminary simulation for light curves of rocket body in LEO. / Hinagawa, Hideaki; Hanada, Toshiya.

:: Advances in the Astronautical Sciences, 巻 148, 01.01.2013, p. 1755-1767.

研究成果: ジャーナルへの寄稿Conference article

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