Trajectory refinement of three-body orbits in the real solar system model

Along with the development, the application can be used as a medium for learning. Augmented Reality is a technology that combines two-dimensional’s virtual objects and three-dimensional’s virtual objects into a real three-dimensional’s then projecting the virtual objects in real time and simultaneously. The introduction of Solar System’s material, students are invited to get to know the planets which are directly encourage students to imagine circumtances in the Solar System. Explenational of planets form and how the planets make the revolution and rotation in books are considered less material’s explanation because its only display objects in 2D. In addition, students can not practice directly in preparing the layout of the planets in the Solar System. By applying Augmented Reality Technology, information’s learning delivery can be clarified, because in these applications are combined the real world and the virtual world. Not only display the material, the application also display images of planets in 3D animation’s objects with audio.

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Implementasi Metode Luther untuk Pengembangan Media Pengenalan Tata Surya Berbasis Virtual Reality

BIOS : Jurnal Teknologi Informasi dan Rekayasa Komputer ◽

10.37148/bios.v1i1.3 ◽

2020 ◽

Vol 1 (1) ◽

pp. 1-14

Author(s):

Adhe Pandhu Dwi Prayogha ◽

Mudafiq Riyan Pratama

Keyword(s):

Virtual Reality ◽

Solar System ◽

Real World ◽

Multimedia Applications ◽

Concept Design ◽

The Real ◽

3 Dimensional ◽

3D Objects ◽

Artificial World ◽

Virtual Reality Application

The purpose of virtual reality is to enable a motor and cognitive sensor activity ofsomeone in the artificial world created digitally to become imaginary, symbolic orsimulate certain aspects in the real world [1]. This technology is applied to the mediaintroduction of the solar system using the Luther method. The Luther Method consistsof 6 stages, namely Concept, Design, Material Collecting, Assembly, Testing, andDistribution. Luther method has advantages compared to other methods because thereare stages of material collecting which is an important stage in the development ofmultimedia and this Luther method can be done in parallel or can go back to theprevious stage [2]. At the Assembly stage the implementation uses the Unity Engineand Google VR SDK for Unity, the result is a virtual reality application that can displaythe solar system with 3-dimensional objects and an explanation is available on eachobject. While testing the blackbox on a variety of Android devices with differentspecifications. From the results of the application of the Luther method, it is verystructured and can run well in the development of multimedia applications, while theresults of testing, this Android-based virtual reality application cannot run on devicesthat do not have Gyroscope sensors and can run on devices with a minimumspecification of 1GB RAM will but the rendering process on 3D objects is slow.

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Load-sharing system model and its application to the real data set

Mathematics and Computers in Simulation ◽

10.1016/j.matcom.2012.02.010 ◽

2012 ◽

Vol 82 (9) ◽

pp. 1615-1629 ◽

Cited By ~ 34

Author(s):

Bhupendra Singh ◽

Puneet Kumar Gupta

Keyword(s):

Real Data ◽

Load Sharing ◽

System Model ◽

Data Set ◽

The Real

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CAPTURE OF DARK MATTER BY THE SOLAR SYSTEM

International Journal of Modern Physics D ◽

10.1142/s0218271809015758 ◽

2009 ◽

Vol 18 (12) ◽

pp. 1903-1912 ◽

Cited By ~ 15

Author(s):

I. B. KHRIPLOVICH ◽

D. L. SHEPELYANSKY

Keyword(s):

Dark Matter ◽

Solar System ◽

Dark Matter Particle ◽

Matter Density ◽

Upper And Lower Bounds ◽

Analytical Estimate ◽

Upper Limits ◽

Galactic Dark Matter ◽

Three Body ◽

Optimistic Value

We study the capture of galactic dark matter by the solar system. The effect is due to the gravitational three-body interaction between the sun, one of the planets, and a dark matter particle. The analytical estimate for the capture cross-section is derived and the upper and lower bounds for the total mass of the captured dark matter particles are found. The estimates for their density are less reliable. The most optimistic of them gives an enhancement of dark matter density by about three orders of magnitudes compared to its value in our galaxy. However, even this optimistic value remains below the best present observational upper limits by about two orders of magnitude.

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Orbits of Trojan Asteroids

Symposium - International Astronomical Union ◽

10.1017/s007418090007039x ◽

1974 ◽

Vol 62 ◽

pp. 63-69 ◽

Cited By ~ 1

Author(s):

G. A. Chebotarev ◽

N. A. Belyaev ◽

R. P. Eremenko

Keyword(s):

Solar System ◽

Body Problem ◽

Equations Of Motion ◽

Orbital Evolution ◽

Restricted Three Body Problem ◽

Three Body Problem ◽

Trojan Asteroids ◽

Actual Motion ◽

Three Body

In this paper the orbital evolution of Trojan asteroids are studied by integrating numerically the equations of motion over the interval 1660–2060, perturbations from Venus to Pluto being taken into account. The comparison of the actual motion of Trojans in the solar system with the theory based on the restricted three-body problem are given.

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Orbital stability of high inclination asteroids

Symposium - International Astronomical Union ◽

10.1017/s0074180900127330 ◽

1996 ◽

Vol 172 ◽

pp. 187-192

Author(s):

N. A. Solovaya ◽

E. M. Pittich

Keyword(s):

Solar System ◽

Body Problem ◽

Equations Of Motion ◽

Orbital Stability ◽

Dynamical Model ◽

Restricted Three Body Problem ◽

Three Body Problem ◽

Three Body

The orbital evolutions of fictitious asteroids with high inclinations have been investigated. The selected initial orbits represent asteroids with movement, which corresponds to the conditions of the Tisserand invariant for C = C (L1) in the restricted three body problem. Initial eccentricities of the orbits cover the interval 0.0–0.4, inclinations the interval 40–80°, and arguments of perihelion the interval 0–360°. The equations of motion of the asteroids were numerically integrated from the epoch March 25, 1991 forward within the interval of 20,000 years, using a dynamical model of the solar system consisting of all planets. The orbits of the model asteroids are stable at least during the investigated period.

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Comparison of Faddeev Method and Resonating Group Method above Breakup Threshold

Zeitschrift für Naturforschung A ◽

10.1515/zna-1975-0301 ◽

1975 ◽

Vol 30 (3) ◽

pp. 271-273 ◽

Cited By ~ 1

Author(s):

F. Söhre ◽

E. W. Schmid

Keyword(s):

Phase Shift ◽

Least Squares ◽

Least Squares Method ◽

Group Method ◽

Breakup Threshold ◽

The Real ◽

Yamaguchi Potential ◽

Three Body

Abstract The reliability of the resonating group method is studied above the three-body breakup threshold. In particular, the real part of the elastic n-d phase shift is calculated in a model of three spinless bosons interacting by a separable Yamaguchi potential for which exact Faddeev results are available. Spurious singularities which are caused by the distortion part of the resonating group ansatz are eliminated by a least squares method.

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