Article
Full entry |
PDF
(2.9 MB)
Feedback
PDF
(2.9 MB)
Feedback
Summary:
The rendezvous realised by the cotangential transfer between two prescribed flightpaths is studied. General formulas based on the two bodies problem are in the conclusion applied to a numerical example calculated for the Earth gravitational field.
References:
[1] П. Е. Эльясберг: Введение в теорию полета искусственных спутников Земли. Наука, Москва 1965. Zbl 1099.01519
[2] К. Mišoň: То the interpretation of the osculations of orbits and the in-space launching point of artificial cosmic bodies. Apl. mat. 14 (1969), 378.
[3] K. Mišoň: La vitesse initiate d'un engin spatial. Czech. Jour. of Phys. B 19 (1969), 1439. DOI 10.1007/BF01690847
[4] K. Mišoň: Rendezvous of satellites describing a common elliptical orbit (with prescribed time of passage through identical positions). Acta Technica (1970), 588.
[5] K. Mišoň: Touching of flightpaths in the problem of two bodies. Acta technica (1971), 553.
[6] H. O. Ruppe: Introduction to astronautics, Vol. I. Academia Press, New York & London 1966. Cited according to:
[7] H. О. Руппе: Введение в астронавтику, Том I. Наука, Москва 1970. Zbl 1107.83313
[8] K. Stumpff: Himmelsmechanik. Bd I. DVW, Berlin 1959.
[9] XXI Symposium de l'U.A.I.: Sur le système de constantes astronomiques. Observatoire de Paris. 27-31. 5. 1965. Cited according to:
[10] Фундаментальные постоянные астрономии. Мир, Москва 1967. Zbl 1103.35360
[11] E. A. Krafft: Space flight. II. dynamics. Nostrand Co, Princeton 1962. Cited according to:
[12] Э. Kpaфт: Космический полет, Том II, динамика. часть первая. Наука, Москва 1969.
Search
Partner of
