scholarly journals Gravity assists near Venus for reaching positions over ecliptic. Resonant asymptotic velocity

2018 ◽  
pp. 1-20
Author(s):  
Yury Filippovich Golubev ◽  
Alexey Vasilyevich Grushevskii ◽  
Victor Vladimirovich Korianov ◽  
Andrey Georgievich Tuchin ◽  
Denis Andreevich Tuchin
2019 ◽  
Vol 484 (3) ◽  
pp. 281-284
Author(s):  
Yu. F. Golubev ◽  
A. V. Grushevskii ◽  
V. V. Koryanov ◽  
A. G. Tuchin ◽  
D. A. Tuchin

An adaptive, semi‑analytical, and geometrically clear method for synthesis of sequences of Venusian gravity‑assist maneuvers setting the desired inclination of a spacecraft orbit is proposed. The geometric constraint on the maximum possible inclination of a spacecraft orbit, which depends on the asymptotic spacecraft velocity relative to Venus, and the dynamic constraint (arising when a gravity‑assist maneuver is performed) on the angle of rotation of the vector of asymptotic velocity relative to Venus are considered simultaneously.


2021 ◽  
Vol 1730 (1) ◽  
pp. 012061
Author(s):  
Alexey Grushevskii ◽  
Yury Golubev ◽  
Victor Koryanov ◽  
Andrey Tuchin ◽  
Denis Tuchin

AIP Advances ◽  
2021 ◽  
Vol 11 (3) ◽  
pp. 035303
Author(s):  
Tatsufumi Nakamura
Keyword(s):  

1998 ◽  
Vol 35 (2) ◽  
pp. 191-198 ◽  
Author(s):  
Roby S. Wilson ◽  
Kathleen C. Howell

2014 ◽  
Vol 37 (2) ◽  
pp. 623-632 ◽  
Author(s):  
Yang Chen ◽  
Hexi Baoyin ◽  
Junfeng Li
Keyword(s):  

2021 ◽  
Vol 30 (1) ◽  
pp. 103-109
Author(s):  
Natan A. Eismont ◽  
Vladislav A. Zubko ◽  
Andrey A. Belyaev ◽  
Ludmila V. Zasova ◽  
Dmitriy A. Gorinov ◽  
...  

Abstract This study discusses the usage of Venus gravity assist in order to choose and reaching any point on Venusian surface. The launch of a spacecraft to Venus during the launch windows of 2029 to 2031 is considered for this purpose. The constraints for the method are the re-entry angle and the maximum possible overload. The primary basis of the proposed strategy is to use the gravitational field of Venus to transfer the spacecraft to an orbit resonant to the Venusian one – with the aim of expanding accessible landing areas. Results of the current research show that this strategy provides an essential increase in accessible landing areas and, moreover, may provide an access to any point on the surface of Venus with a small increase in ∆V required for launch from the Earth and in the flight duration. The comparison with the landing without using gravity assist near planet is also given.


Author(s):  
Andreas Knauf

Asymptotic velocity is defined as the Cesàro limit of velocity. As such, its existence has been proved for bounded interaction potentials. This is known to be wrong in celestial mechanics with four or more bodies. Here, we show for a class of pair potentials including the homogeneous ones of degree − α for α ∈(0, 2), that asymptotic velocities exist for up to four bodies, dimension three or larger, for any energy and almost all initial conditions on the energy surface. This article is part of the theme issue ‘Finite dimensional integrable systems: new trends and methods’.


2021 ◽  
Vol 0 (0) ◽  
pp. 0
Author(s):  
Giovanni Colombo ◽  
Paolo Gidoni ◽  
Emilio Vilches

<p style='text-indent:20px;'>We study the asymptotic stability of periodic solutions for sweeping processes defined by a polyhedron with translationally moving faces. Previous results are improved by obtaining a stronger <inline-formula><tex-math id="M1">\begin{document}$ W^{1,2} $\end{document}</tex-math></inline-formula> convergence. Then we present an application to a model of crawling locomotion. Our stronger convergence allows us to prove the stabilization of the system to a running-periodic (or derivo-periodic, or relative-periodic) solution and the well-posedness of an average asymptotic velocity depending only on the gait adopted by the crawler. Finally, we discuss some examples of finite-time versus asymptotic-only convergence.</p>


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