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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.14 Number.2
- 발행연도
- 2013.6
- 수록면
- 193 - 199 (7page)
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초록· 키워드
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This work investigates the orbital perturbations of the cubesats that lie on LEO due to Earth albedo. The motivation for this paper originated in the investigation of the orbital perturbations for closed- Earth pico-satellites due to the sunlight reflected by the Earth (the albedo). Having assumed that the Sun lies on the equator, the albedo irradiance is calculated using a numerical model in which irradiance depends on the geographical latitude, longitude and altitude of the satellite. However, in the present work the longitude dependency is disregarded. Albedo force and acceleration components are formulated using a detailed model in a geocentric equatorial system in which the Earth is an oblate spheroid. Lagrange planetary equations in its Gaussian form are used to analyze the orbital changes when e≠0 and i≠0 . Based on the Earth’s reflectivity data measured by NASA Total Ozone Mapping Spectrometer (TOMS project), the orbital perturbations are calculated for some cubesats. The outcome of the numerical test shows that the albedo force has a significant contribution on the orbital perturbations of the pico-satellite which can affect the satellite life time.
목차
Abstract
1. Introduction
2. Numerical Application
3. Conclusion
4. Future work
References
참고문헌 (18)
참고문헌 신청
1. [학술대회논문] - Ali Ravanbakhsh / 2010 / Preliminary Structural Sizing of a Modular Microsatellite Based on System Engineering Considerations / Third International Conference on Multidisciplinary Design Optimization and Applications
2. [학술지(정기간행물)] - Anselmo L. / 1983 / Effects of the Earth Reflected Sunlight on the Orbit of the LAGEOs Satellite / Astronomy and Astrophysics 117 (1) : 1 ~ 3
3. [학술지(정기간행물)] - Antreasian, P. G. / 1992 / Prediction of radiant energy forces on the TOPEX/POSEIDON spacecraft / Journal of Spacecraft and Rockets 2 (1) : 81 ~ 90
4. [학위논문] - Bhanderi D.D.V. / 2005 / Spacecraft attitude determination with Earth albedo corrected Sun sensor measurements / 박사 / Aalborg University
5. [학술대회논문] - Bhanderi D.D.V. / 2005 / Modeling Earth Albedo for Satellites in Earth Orbit / AIAA Guidance, Navigation, and Control Proceedings
2. [학술지(정기간행물)] - Anselmo L. / 1983 / Effects of the Earth Reflected Sunlight on the Orbit of the LAGEOs Satellite / Astronomy and Astrophysics 117 (1) : 1 ~ 3
3. [학술지(정기간행물)] - Antreasian, P. G. / 1992 / Prediction of radiant energy forces on the TOPEX/POSEIDON spacecraft / Journal of Spacecraft and Rockets 2 (1) : 81 ~ 90
4. [학위논문] - Bhanderi D.D.V. / 2005 / Spacecraft attitude determination with Earth albedo corrected Sun sensor measurements / 박사 / Aalborg University
5. [학술대회논문] - Bhanderi D.D.V. / 2005 / Modeling Earth Albedo for Satellites in Earth Orbit / AIAA Guidance, Navigation, and Control Proceedings
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