Abstract:This paper deals with generation of halo orbits in the three-dimensional photogravitational restricted three-body problem, where the more massive primary is considered as the source of radiation and the smaller primary is an oblate spheroid with its equatorial plane coincident with the plane of motion. Both the terms due to oblateness of the smaller primary are considered. Numerical as well as analytical solutions are obtained around the Lagrangian point L1, which lies between the primaries, of the Sun-Earth s… Show more
“…Halo orbits are important for spacecraft mission design. Many researchers have obtained the halo orbits upto third order approximation (Richardson 1980;Howell 1984;Breakwell and Brown 1979;Koon et al 2011;Chidambararaj and Sharma 2016;Pushparaj and Sharma 2016;Ghotekar and Sharma 2019). Tiwary and Kushvah (2015) have computed halo orbits upto fourth order approximation with the Sun as a radiating body and the Earth as an oblate spheroid using Lindstedt-Poincaré method.…”
Section: Lindstedt-poincaré Methods For the Halo Orbitsmentioning
The Photogravitational Restricted Three Body Problem with oblateness has been studied to obtain halo orbits around the Lagrangian points L 1 and L 2 of the Sun-Earth system in which the Sun is taken as radiating and the Earth as an oblate spheroid. The halo orbits corresponding to fourth and fifth order approximations around L 1 and L 2 for actual oblateness of the Earth and for different radiation pressures for the Sun are displayed graphically. The time period of halo orbits around L 1 decreases with increase in oblateness and increases with increase in radiation pressure. A reverse effect is observed due to increase in oblateness and radiation pressure on time period of orbits around L 2 . It is also observed that halo orbits around L 1 shifts towards the source of radiation due to increase in both radiation pressure and oblateness. However, halo orbits around L 2 shifts towards the source of radiation due to increase in radiation but recedes with increase in oblateness.
“…Halo orbits are important for spacecraft mission design. Many researchers have obtained the halo orbits upto third order approximation (Richardson 1980;Howell 1984;Breakwell and Brown 1979;Koon et al 2011;Chidambararaj and Sharma 2016;Pushparaj and Sharma 2016;Ghotekar and Sharma 2019). Tiwary and Kushvah (2015) have computed halo orbits upto fourth order approximation with the Sun as a radiating body and the Earth as an oblate spheroid using Lindstedt-Poincaré method.…”
Section: Lindstedt-poincaré Methods For the Halo Orbitsmentioning
The Photogravitational Restricted Three Body Problem with oblateness has been studied to obtain halo orbits around the Lagrangian points L 1 and L 2 of the Sun-Earth system in which the Sun is taken as radiating and the Earth as an oblate spheroid. The halo orbits corresponding to fourth and fifth order approximations around L 1 and L 2 for actual oblateness of the Earth and for different radiation pressures for the Sun are displayed graphically. The time period of halo orbits around L 1 decreases with increase in oblateness and increases with increase in radiation pressure. A reverse effect is observed due to increase in oblateness and radiation pressure on time period of orbits around L 2 . It is also observed that halo orbits around L 1 shifts towards the source of radiation due to increase in both radiation pressure and oblateness. However, halo orbits around L 2 shifts towards the source of radiation due to increase in radiation but recedes with increase in oblateness.
“…The variation in size, shape of the halo orbits is observed by comparing it with the plots of classical case and the effects of radiation pressures on the halo orbit is observed. The numerical computation of halo orbits is referred from Chidambararaj P. and Sharma R. K. [14].…”
Section: Numerical Computation Of Halo Orbitsmentioning
We study halo orbits in the circular restricted three-body problem (CRTBP) with both the primaries as the sources of radiation. The positioning of the triangular equilibrium points is discussed in a rotating coordinate system.
“…5 shows that the time delay in this time series is modulated with a periodicity of almost 6 months. This is due to the SoHO halo orbit 9 , which has a periodicity of 178 days resulting in a time modulation of 1.54 s. The periodicity of 178 days is primarily constrained by the solar radiation pressure (Chidambararaj & Sharma 2016).…”
Context. The recent claims of g-mode detection have restarted the search for these potentially extremely important modes. These claims can be reassessed in view of the different data sets available from the SoHO instruments and ground-based instruments. Aims. We produce a new calibration of the GOLF data with a more consistent p-mode amplitude and a more consistent time shift correction compared to the time series used in the past. Methods. The calibration of 22 years of GOLF data is done with a simpler approach that uses only the predictive radial velocity of the SoHO spacecraft as a reference. Using p modes, we measure and correct the time shift between ground-and space-based instruments and the GOLF instrument. Results. The p-mode velocity calibration is now consistent to within a few percent with other instruments. The remaining time shifts are within ± 5 s for 99.8% of the time series.
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