Zhuravlev, S. G.; Anikovsky, V. V. Expansion of the perturbing function of a satellite restricted four-body problem. (English) Zbl 0473.70023 Celestial Mech. 24, 237-254 (1981). Page: −5 −4 −3 −2 −1 ±0 +1 +2 +3 +4 +5 Show Scanned Page MSC: 70M20 Orbital mechanics 70F10 \(n\)-body problems 85A99 Astronomy and astrophysics 70F15 Celestial mechanics Keywords:expansion perturbing function; artificial satellite; two perturbing bodies; inclination of the orbits; accuracy of 19th order; eccentricities of orbits Citations:Zbl 0397.34050 PDFBibTeX XMLCite \textit{S. G. Zhuravlev} and \textit{V. V. Anikovsky}, Celest. Mech. 24, 237--254 (1981; Zbl 0473.70023) Full Text: DOI References: [1] Jarnagin, M. P. Jr.: 1968,Astron. Papers 18, 1. [2] Zhuravlev, S. G.: 1972a, ?Analytical Theory of Motion of a Synchronous Earth’s Satellite. Part 1. Intermediate Orbit?,Mezhved. Sbornic Problemi mekhanici upravlyaemogo dvizheniya, Perm, pp., 68?84. [3] Zhuravlev, S. G.: 1972b, ?Analytical Theory of Motion of a Synchronous Earth’s Satellite. Part 2. Secular, Long-Periodic and Short-Periodic Perturbations?,Mezhved. Sbornic Problemi mekhanici upravlyaemogo dvizheniya, Perm, pp. 85?99 [4] Zhuravlev, S. G.: 1975,Astron. J. 52, 6. [5] Zhuravlev, S. G.: 1976,Mezhved. sbornic Matematicheskaya phisica, Kiev 20, 17. [6] Zhuravlev, S. G.: 1979,Celest. Mech. 19, 77. · Zbl 0397.34050 · doi:10.1007/BF01230176 This reference list is based on information provided by the publisher or from digital mathematics libraries. Its items are heuristically matched to zbMATH identifiers and may contain data conversion errors. In some cases that data have been complemented/enhanced by data from zbMATH Open. This attempts to reflect the references listed in the original paper as accurately as possible without claiming completeness or a perfect matching.