Six-impulse maneuvers for rendezvous of spacecraft in near-circular noncoplanar orbitsSpringer Science and Business Media LLC - Tập 50 - Trang 441-448 - 2012
A. A. Baranov, D. S. Roldugin
The problem of a rendezvous of two spacecraft in close near-circular noncoplanar orbits is considered. The angles of applying velocity impulses and their orientation are determined from necessary conditions of optimality derived using the basis vector theory. For non-degenerate six-impulse solutions the analytical formulas are found that approximate the dependence of moments of applying velocity i...... hiện toàn bộ
Families of Periodic Solutions to the Beletsky EquationSpringer Science and Business Media LLC - - 2002
A. D. Bruno
A review of achievements in the investigation of the planar periodic oscillations and rotations of a satellite around its center of mass, which moves along an elliptic orbit in the central gravitational field, is presented. These oscillations and rotations of the satellite are described by an ordinary differential equation (Beletsky equation) of the second order with periodic coefficients and two ...... hiện toàn bộ
Magneto-ionospheric effects of active experiments conducted on February 18, 2004Springer Science and Business Media LLC - Tập 49 - Trang 292-307 - 2011
L. F. Chernogor
Results of radiophysical and magnetometric observations of dynamical processes in the ionosphere and geomagnetic field that followed launches of four rockets of different power and made from different launching sites are analyzed. It is found that the rocket launches were accompanied by an intensification of wave activity in the ionosphere and geomagnetic field. The medium reactions from various s...... hiện toàn bộ
A Technique for Estimating the Space Debris Density from the Data of Onboard Recording SystemsSpringer Science and Business Media LLC - Tập 41 - Trang 204-208 - 2003
V. V. Mironov
A three-dimensional mathematical model and a program complex for modeling the external effect of small-sized space debris particles on a spacecraft are developed. On the basis of the rectangular contributions method a new technique is developed for restoring the density of small-sized space debris from a small number of recorded debris collisions with recording sensors. From the form of the densit...... hiện toàn bộ
Stationary Nose Structures of Protons in the Inner Magnetosphere: Observations by the ION Instrument onboard the Interball-2 Satellite and ModelingSpringer Science and Business Media LLC - Tập 41 - Trang 3-12 - 2003
N. Yu. Buzulukova, R. A. Kovrazhkin, A. L. Glazunov, J.-A. Sauvaud, N. Yu. Ganushkina, T. I. Pulkkinen
Nose structures are objects formed by H+ particles penetrating into the inner magnetosphere [1, 2]. We present the results of experimental studies and numerical modeling of the nose structures. Statistical processing of the observations of nose structures in 1997 by the ION instrument onboard the Interball-2 satellite at heights of 10 000–15 000 km demonstrates that the probability of formation of...... hiện toàn bộ
Determination of two Satellites’ relative motion using tracking measurementsSpringer Science and Business Media LLC - Tập 46 - Trang 523-528 - 2008
M. Yu. Ovchinnikov, S. S. Tkachev
A technique to determine the initial relative velocity of two satellites at the initial time instant, based on the results of NORAD system’s measurements, is presented. The determination of a relative initial position is shown to result in the unsatisfactory accuracy. This technique is applied to determining the initial velocity of separation of the first Russian nanosatellite TNS-0 from the Inter...... hiện toàn bộ