[PDF] Top 20 Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits
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Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits
... the problem and the equations of motion of the solar sail, as well as the equilibrium ...periodic orbits, and in Section 5 we examine the invariant manifolds of equilibria and periodic ... See full document
13
Control of Lagrange point orbits using solar sail propulsion
... utilises solar radiation pressure to provide a useful thrust. The sail is a thin reflective film with a thickness of order 2 μm, with a large reflective area in order to intercept a flux of ...of ... See full document
11
Solar Sail Equilibrium Orbits in the Circular Restricted Three Body Problem with Oblateness
... investigate solar sail in the circular restricted three-body problem, where the larger primary is a source of radiation and the smaller primary is an oblate spheroid in the ...for ... See full document
10
Solar sail Lyapunov and halo orbits in the Earth-Moon three-body problem
... a solar sail, to the CR3BP complements these five Lagrange points with an infinite set of artificial equilibrium points ...periodic orbits around these AEPs [7] have been suggested for ... See full document
18
Solar sail orbits at the Earth-Moon libration points
... the sail is pitched from γ = 0 at t = 0, the motion of the sail is of the form of periodic oscillations at an out-of plane given ...the sail remains at this fixed distance. It was found that periodic ... See full document
11
Invariant manifolds and orbit control in the solar sail three-body problem
... of solar sails in the circular restricted Earth-Sun system. Fixed points for solar sails in this system have the linear dynamical properties of saddles crossed with centers; thus the fixed ... See full document
15
Solar sail heliocentric Earth-following orbits
... Solar sail technology development is rapidly gaining momentum after recent successes such as JAXA’s IKAROS mission [1] and NASA’s NanoSail-D2 mission ...new solar sail initiatives, such as ... See full document
19
New periodic orbits in the solar sail restricted three body problem
... The characteristic equation of the Jacobian A is bi-cubic (whose cor- responding cubic equation has real roots); this means the eigenvalues of A are either in pairs of pure imaginary conjugates or real and of opposite ... See full document
11
Non-Keplerian orbits using hybrid solar sail propulsion for Earth applications
... of solar sails and SEP, Leipold and Götz 88 proposed a hybridisation of the two systems on the same ...small solar sails will be required, the hybridisation lowers the solar sail AD 2 ... See full document
275
Solar sail periodic orbits in the Earth-Moon three-body problem
... Sun-Earth three-body problem, while little research has been conducted to investigate the potential of solar sailing in the Earth-Moon three-body ...find solar sail ... See full document
11
New periodic orbits in the solar sail three-body problem
... The characteristic equation of the Jacobian A is bi-cubic (whose cor- responding cubic equation has real roots); this means the eigenvalues of A are either in pairs of pure imaginary conjugates or real and of opposite ... See full document
12
Solar sail formation flying for deep-space remote sensing
... term solar sail with β = ...the solar sail circular (e = 0) restricted three body ...equilibrium points are then used as a starting point to generate periodic ... See full document
16
Halo Orbits in the Photo Gravitational Restricted Three Body Problem
... Halo Orbits have been the topic of interest for the past few decades among the research ...periodic, three-dimensional orbit around the Lagrangian points in a three-body ...Halo ... See full document
18
Agile solar sailing in three-body problem : Motion between artificial equilibrium points
... the sail normal vector as if each position along the initial guess were an AEP, the initial guess needs to circumvent the white, forbidden sail ...the sail passes below and ‘behind’ the Earth in its ... See full document
13
Solar sail trajectories at the Earth-Moon Lagrange points
... non-Keplerian orbits, such as closed orbits displaced high above the eclip- tic plane (see Waters and McInnes ...[2]). Solar sails are es- pecially suited for such non-Keplerian orbits, since ... See full document
7
Displaced periodic orbits with low-thrust propulsion
... the sail attitude is fixed such that the sail normal vector n , which is the unit vector that is perpendicular to the sail surface, points always along the direction of the Sun line with the ... See full document
15
Designing displaced lunar orbits using low-thrust propulsion
... the nonlinearities and to impose desired linear dynamics satisfied by the solar sail. We then select the SEP control, which takes into consideration the nonlinearity cancellation and the stabilizing ... See full document
11
Orbits in a generalized two-body problem
... and solar gravity have an inverse square variation, the induced thrust can be parameterized by the lightness number ¯, de ned as the ratio of the thrust force to solar gravitational force acting on the ... See full document
8
Periodic Orbits around Triangular Points in the Restricted Problem of Three Oblate Bodies
... The restricted three-body (RTBP) has been generalized in the past years to include the case when one or both primaries are radiation source. Studies of this kind include among many, Radzievskii [8], Simmons ... See full document
5
Design and applications of solar sail periodic orbits in the non-autonomous Earth-Moon system
... To assess the potential of the out-of-plane flower-shaped orbits for high-latitude observation, the motion of the Earth’s polar axis needs to be described in the synodic frame. For this, the small inclination ... See full document
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