Abstract
A highly accurate algorithm for synthesizing chains of cranking gravity-assist maneuvers (GAMs) has been constructed using formalization of the search for ballistic scenarios followed by the adaptive involvement of tens of millions of variants. Its use results in a significant change in the orbital inclination of a research spacecraft without a significant expenditure of propellant with a reasonable mission time.
Similar content being viewed by others
References
Yu. F. Golubev, A. V. Grushevskii, V. V. Koryanov, and A. G. Tuchin, Synthesis of space mission scenarios in the Jovian system using Gravity Assist Maneuvers, Dokl. Phys. 59 (5), 226 (2014).
Yu. F. Golubev, A. V. Grushevskii, V. V. Koryanov, A. G. Tuchin, and D. A. Tuchin, Bifurcation points during Gravity Assist Tours in the Jovian system, Dokl. Phys. 60 (5), 210 (2015).
A. V. Grushevskii, Yu. F. Golubev, V. V. Koryanov, and A. G. Tuchin, Adaptive Low Radiation Multibody Gravity Assist Tours Design in Jovian System for the Landing on Jovian’s Moons in Proc. 65th IAC. Toronto, 2014, Manuscript IAC-14-C1.9.13.
A. V. Labunsky, O. V. Papkov, and K. G. Sukhanov, Multiple Gravity Assist Interplanetary Trajectories in ESI Book Series. L.: Gordon and Breach Publ., 1998, pp. 9–266.
Yu. F. Golubev, A. V. Grushevskii, V. V. Koryanov, A. G. Tuchin, and D. A. Tuchin, On the Variation in the Orbital Inclination of Celestial Bodies when Executing a Gravity-Assist Maneuver in the Solar System, Prepr. Keldysh Inst. Appl. Math., No. 15 (2016) [in Russian].
Yu. F. Golubev, A. V. Grushevskii, V. V. Koryanov, A. G. Tuchin, and D. A. Tuchin, Technique for Designing Highly Inclined Spacecraft Orbits Using Gravity- Assist Maneuvers, Prepr. Keldysh Inst. Appl. Math., No. 64 (2015) [in Russian].
N. J. Strange, R. Russell, and B. Buffington, Mapping the V-Infinity Globe in AIAA/AAS Space Flight Mechanics Meeting, AAS Pap. 07-277, Sedona (AZ) (2007).
Y. Kawakatsu, Direction Diagram and Its Application to Swingby Design., XXI ISSFD, Toulouse (2009).
J. M. S. Pérez, Trajectory Design of Solar Orbiter, XXIII ISSFD, Pasadena (2012).
M. Konstantinov, V. Petukhov, and M. Thein, Optimization Spacecraft Insertion into the System of Heliocentric Orbits for Sun Exploration, 65th IAC, Toronto, IAC-14-C1.9.4 (2014).
S. Campagnola and Y. Kawakatsu, J. Spacecraft and Rockets 49 (2), 318 (2012).
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © Yu.F. Golubev, A.V. Grushevskii, V.V. Koryanov, A.G. Tuchin, D.A. Tuchin, 2017, published in Doklady Akademii Nauk, 2017, Vol. 472, No. 4, pp. 403–406.
Rights and permissions
About this article
Cite this article
Golubev, Y.F., Grushevskii, A.V., Koryanov, V.V. et al. A technique for designing highly inclined spacecraft orbits using gravity-assist maneuvers. Dokl. Phys. 62, 76–79 (2017). https://doi.org/10.1134/S1028335817020033
Received:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S1028335817020033