Results 1 to 10 of about 109,132 (281)
Científica, 2022 There are different ways to solve motion problems, namely, Newtonian, Lagrangian, Hamiltonian, powerful methods in solving any problem related to motion and its possible causes.
Mario Antonio Ramirez Flores +1 more
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Asymptotic analysis of displaced lunar orbits [PDF]
, 2009 The design of spacecraft trajectories is a crucial task in space mission design. Solar sail technology appears as a promising form of advanced spacecraft propulsion which can enable exciting new space science mission concepts such as solar system ...
Simo, Jules, McInnes, Colin R.
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Artificial halo orbits for low-thrust propulsion spacecraft [PDF]
, 2009 We consider periodic halo orbits about artificial equilibrium points near to the Lagrange points L1 and L2 in the circular restricted three-body problem, where the third body is a low-thrust propulsion spacecraft in the Sun-Earth system.
Baig, Shahid, McInnes, Colin R.
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New periodic orbits in the solar sail three-body problem [PDF]
, 2011 We identify displaced periodic orbits in the circular restricted three-body problem, wher the third (small) body is a solar sail. In particular, we consider solar sail orbits in the earth-sun system which are high above the exliptic plane.
Biggs, J.D., Waters, T., McInnes, C.R.
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Izviđanje satelitskih komunikacija u funkciji savremenih operacija / Reconnaissance of satellite communications in contemporary operations [PDF]
Vojnotehnički Glasnik, 2004 Raspoloživi vojni resursi u bilo kojoj kategoriji nisu kritični u mirnodopskom periodu, jer se dimenzionišu za ratno naprezanje određenog nivoa. Međutim, u uslovima izvođenja borbenih dejstava postoje ekstremi u zahtevima za angažovanjem, koje sistemi ne
Slaviša Đukanović
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Remote Sensing, 2021 The present study aims to investigate the potential of multi-configuration Sentinel-1 (S-1) synthetic aperture radar (SAR) images for characterizing four wheat parameters: total fresh mass (TFM), total dry mass (TDM), plant heights (He), and water ...
Azza Gorrab +3 more
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Displaced solar sail orbits : dynamics and applications [PDF]
, 2010 We consider displaced periodic orbits at linear order in the circular restricted Earth-Moon system, where the third massless body is a solar sail. These highly non-Keplerian orbits are achieved using an extremely small sail acceleration.
Simo, Jules, McInnes, Colin R.
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On the Dynamic Geometry of Kasner Quadrilaterals with Complex Parameter
Mathematics, 2022 We explore the dynamics of the sequence of Kasner quadrilaterals (AnBnCnDn)n≥0 defined via a complex parameter α. We extend the results concerning Kasner triangles with a fixed complex parameter obtained in earlier works and determine the values of α for
Dorin Andrica, Ovidiu Bagdasar
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Computation of Zagreb and atom-bond connectivity indices of certain families of dendrimers by using automorphism group action [PDF]
Journal of the Serbian Chemical Society, 2017 In QSAR/QSPR studies, topological indices are utilized to predict the bioactivity of chemical compounds. In this paper, the closed forms of different Zagreb indices and atom–bond connectivity indices of regular dendrimers G[n] and H[n] in terms of a ...
Ahmad Uzma, Ahmad Sarfraz, Yousaf Rabia
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On the stability of displaced two-body lunar orbits [PDF]
, 2010 In a prior study, a methodology was developed for computing approximate large displaced orbits in the Earth-Moon circular restricted three-body problem (CRTBP)by the Moon-Sail two-body problem.
Simo, Jules, McInnes, Colin R.
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