Suryadi Siregar
Astronomy Research Division And Bosscha Observatory, Faculty Of Mathematics And Natural Sciences, ITB

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Recalculating the Orbit of α-Centauri AB Suryadi Siregar; Hanindyo Kuncarayakti
Jurnal Matematika & Sains Vol 12, No 3 (2007)
Publisher : Institut Teknologi Bandung

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Abstract

The two main components of the closest star system, α Centauri AB (RA 14h39m, Dec -60o50, J2000.0) is indubitablyone of the most studied visual double stars. This paper presents the results of our recalculation of orbital and physicalparameters of the system using Thiele-van den Bos method, based on observational data from year 1900 to 2002.Despite some significant discrepancies, in general our results confirmed previous results of orbital parameterdeterminations using different method.
Migration of Near Earth Asteroid to Jovian-Crosser Asteroid : Case Study 3552 Don Quixote Suryadi Siregar
Jurnal Matematika & Sains Vol 15, No 1 (2010)
Publisher : Institut Teknologi Bandung

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Abstract

It is generally recognized that main-belt asteroids (MBAs) and nuclei of extinct comets are the two main sources for the Near-Earth-Asteroids (NEAs). Theoretical studies of NEAs dynamics and numerical modelling of their orbital motions showed that the resonance mechanism for supplying NEAs is quite sufficient to sustain this population. Asteroid 1983 SA, also known as 3552 Don Quixote, is one of Near Earth Asteroids (NEAs) and the most probable candidates for NEAs of the cometary origin. In this work, an investigation on the evolution of the orbit is done by using the SWIFT subroutine package, where the gravitational perturbations of eight planets: Mercury, Venus, Earth, Mars, Jupiter, Saturn, Uranus, and Neptune are considered. Migration of asteroid 3552 Don Quixote from Near Earth Asteroids (NEAs) to Jovian-crosser asteroid is found.
Will 3552 Don Quixote Escape from the Solar System? Suryadi Siregar
Journal of Mathematical and Fundamental Sciences Vol. 43 No. 3 (2011)
Publisher : Institute for Research and Community Services (LPPM) ITB

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.5614/itbj.sci.2011.43.3.4

Abstract

Asteroid 1983 SA, well known as 3552 Don Quixote, is one of Near Earth Asteroids (NEAs) which is the most probable candidate for the cometary origin, or otherwise as Jupiter-Family-Comets (JFCs). The aim of this study is to investigate the possibility of 3552 Don Quixote to be ejected from the Solar System. This paper presents an orbital evolution of 100 hypothetical asteroids generated by cloning 3552 Don Quixote. Investigation of its orbital evolution is conducted by using the SWIFT subroutine package, where the gravitational perturbations of eight major planets in the Solar System are considered. Over very short time scales (220 kyr) relative to the Solar System life time (10 Gyr), the asteroid 3552 Don Quixote gave an example of chaotic motion that can cause asteroid to move outward and may be followed by escaping from the Solar System. Probability of ejection within the 220 kyr time scale is 50%.
TELAAH AWAL KEUBAHAN SETENGAH SUMBU PANJANG AKIBAT EFEK YARKOVSKY PADA ASTEROID 3362 KHUFU (1984 QA) Endang Soegiartini; Suryadi Siregar
Jurnal Sains Dirgantara Vol 5, No 2 (2008)
Publisher : Lembaga Penerbangan dan Antariksa Nasional

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Abstract

Efek Yarkovsky adalah gaya non-gravitasional yang bekerja pada benda yang disebabkan oleh emisi anisotropik foton termal, yang memberi momentum bagi benda tersebut. Efek ini biasanya terjadi pada meteoroid atau asteroid berukuran kecil (dengan diameter 10 cm sampai 10 km). Tulisan ini mencoba meninjau efek Yarkovsky tersebut bagi asteroid 3362 Khufu (1984 QA) yang berdiameter 0.7 km, serta Bond-albedo 0.17. Efek Yarkovsky menyebabkan keubahan pada setengah sumbu panjang orbit, akibatnya eksentrisitas orbit juga berubah. Terjadinya perubahan pada elemen orbit memberikan peluang asteroid tersebut bergerak mendekati Bumi. Telaah ini menunjukkan amplitudo keubahan setengah sumbu panjang orbit terhadap waktu akibat komponen harian dan musiman, masing-masing maksimal adalah 1.3×10-5 m/detik dan -3.7×10-9 m/detik. Kata kunci: Efek Yarkovsky, Asteroid, Orbit.