[PDF] Top 20 Periodic orbits high above the ecliptic plane in the solar sail 3-body problem
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Periodic orbits high above the ecliptic plane in the solar sail 3-body problem
... Solar Sails 3 Body Equations and Equilibria Periodic Solutions Outline 1 Solar Sails Sail design 2 3 Body Equations and Equilibria Classical equilibria - the Lagrange points Sail equilib[r] ... See full document
37
Stabilizing periodic orbits above the elliptic plane in the solar sail 3-body problem
... applicable above the ecliptic in the SSETBP as there are no equilibrium points in this ...for periodic orbits above the ecliptic ...a periodic orbit above the ... See full document
7
Solar sail Lyapunov and halo orbits in the Earth-Moon three-body problem
... planar solar sail Lyapunov orbit with = 0 and a 0,EM ...of orbits that results from this is provided in Figure 9a-b for a range of pitch angles, 60, 60 in ...the orbits for ... See full document
18
Displaced periodic orbits with low-thrust propulsion
... and solar electric technology provide alternative forms of space- craft ...as solar system exploration and deep space ...three-body problem (CRTBP), where the third massless body ... See full document
15
Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits
... system’s periodic orbits and invariant ...of solar sails in the ...describe periodic orbits about equilibrium points in the solar sail three body problem, ... See full document
13
Solar Sail Equilibrium Orbits in the Circular Restricted Three Body Problem with Oblateness
... three-body problem (RTBP) has been considered a basic dynamic model ever since the scien- tists have studied the solar sail [12] ...tellite, solar sail or asteroid, moving under ... See full document
10
Displaced solar sail orbits : Dynamics and applications
... displaced periodic orbits at linear order in the circular restricted Earth- Moon system, where the third massless body is a solar ...non-Keplerian orbits are achieved using an extremely ... See full document
11
Solar sail orbits at the Earth-Moon libration points
... Solar sail technology offer new capabilities for the analysis and design of space ...non-Keplerian orbits for solar sail spacecraft at linear order are investigated in the Earth-Moon ... See full document
11
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
Displaced solar sail orbits : dynamics and applications
... displaced periodic orbits at linear order in the circular restricted Earth- Moon system, where the third massless body is a solar ...non-Keplerian orbits are achieved using an extremely ... See full document
11
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 families of Sun-centred non-Keplerian orbits over cylinders and spheres
... non-Keplerian orbits (NKOs) that are confined to a two-dimensional plane (also referred to as ”z- static” NKOs), this paper has introduced Sun-centred NKOs that are con- strained to a three-dimensional ... See full document
38
Invariant manifolds and orbit control in the solar sail three-body problem
... and periodic orbits, and presenting the controllability of each would be tedious and distract from the overall ...x-z plane is specified by the parameters (β, ...and 3) this precise value was ... See full document
15
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
On the a and g families of orbits in the Hill problem with solar radiation pressure and their application to asteroids
... large solar radiation pressure perturbation (SRP) on spacecraft dynamics is of great importance for asteroid exploration ...of periodic solutions propagated with a numerical integrator considering the ... See full document
21
Design and applications of solar sail periodic orbits in the non-autonomous Earth-Moon system
... flower-shaped orbits for high-latitude observation, the motion of the Earth’s polar axis needs to be described in the synodic ...the ecliptic, eq , and the fact that the Earth’s polar axis is ... See full document
20
Control of solar sail periodic orbits in the elliptic three-body problem
... suitable periodic reference trajectories above the ecliptic for the solar sail ...orbit above the ecliptic in the solar sail ... See full document
6
New periodic orbits in the solar sail three-body problem
... dinate system in which the primary masses are fixed on the x-axis with the origin at the centre of mass, the z-axis is the axis of rotation and the y-axis completes the triad. We choose our units to set the gravitational ... See full document
12
Solar sail formation flying for deep-space remote sensing
... term solar sail with β = ...McInnes 3 a plot of the artificial equilibria above the ecliptic for different values of β are given for the case of the solar sail circular (e ... See full document
16
Solar sail periodic orbits in the Earth-Moon three-body problem
... 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 periodic ... See full document
11
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