[PDF] Top 20 Control of solar sail periodic orbits in the elliptic three-body problem
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Control of solar sail periodic orbits in the elliptic three-body problem
... the solar sail lightness number and is the ratio of the solar sail radiation pressure acceleration to the solar gravitational acceleration, the ‘hat’ notation denotes the unit vector ... See full document
6
Design and applications of solar sail periodic orbits in the non-autonomous Earth-Moon system
... the solar sail eight-shaped orbit constellation requires fewer satellites to establish a continuous view, while it requires more satellites than the single South Pole-sitter sailcraft proposed in ...complex ... See full document
20
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 ...addition, periodic orbits around these AEPs [7] have been suggested ... See full document
18
Stabilizing periodic orbits above the elliptic plane in the solar sail 3-body problem
... consider periodic orbits high above the ecliptic plane in the Elliptic Restricted Three-Body Problem where the third massless body is a solar ...sail. ... See full document
7
Solar sail periodic orbits in the Earth-Moon three-body problem
... the solar sail normal vector changes sign when the Sun moves from a position where it illuminates the Earth-facing side of the sail to a position where it illuminates the Moon-facing side of the ... See full document
11
Designing displaced lunar orbits using low-thrust propulsion
... displaced periodic orbits at linear order in the circular restricted Earth-Moon system, where the third massless body utilizes a hybrid of solar sail and a solar electric ... See full document
11
Invariant manifolds and orbit control in the solar sail three-body problem
... of solar sails. In particular, the solar sail in the setting of the circular restricted 3-body problem (CR3BP) has produced new and interesting families of orbits which are ... See full document
15
Solar Sail Equilibrium Orbits in the Circular Restricted Three Body Problem with Oblateness
... restricted three-body problem with the larger primary a source of radiation and the smaller primary an ob- late spheroid is ...restricted three-body problem in Figure ... See full document
10
Displaced periodic orbits with low-thrust propulsion
... and solar electric technology provide alternative forms of space- craft ...as solar system exploration and deep space ...restricted three-body problem (CRTBP), where the third massless ... See full document
15
Solar sail equilibria in the elliptical restricted three-body problem
... in three-dimensional space, in the non-uniformly rotating, pulsating coordinate ...a control scheme for the stabilization of out-of-plane equilibria will be derived for the small eccentricity ...restricted ... See full document
27
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
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 Radiation Pressure Effects on Stability of Periodic Orbits in Restricted Four Body Problem
... four-body problem has an important role in astro-dynamics and space dynamics, therefore many attempts dealing with this problem have been done using numerical and analytical ...four-body ... See full document
14
Extension of Earth-Moon libration point orbits with solar sail propulsion
... restricted three-body problem with a solar ...the solar sail induced acceleration, families of Lyapunov, halo, ver- tical Lyapunov, Earth-centred, and distant retrograde ... See full document
20
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
... a three-dimensional, cylindrical or spherical ...spherical orbits are found by investigating the geometri- cally constrained spacecraft ...feasible orbits is defined. Additionally, the phase spaces ... See full document
38
New periodic orbits in the solar sail restricted three body problem
... The Newton method starts with an orbit X (t) initialized at t = 0 on a surface of section. In our case we require that the orbit be exactly 1 year so the return map in the rotating-pulsating frame is defined by a T-map ... See full document
11
New periodic orbits in the solar sail three-body problem
... The Newton method starts with an orbit X(t) initialized at t = 0 on a surface of section. In our case we require that the orbit be exactly 1 year so the return map in the rotating-pulsating frame is defined by a T-map of ... See full document
12
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
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 ...to periodic orbits, and in Section 5 we examine the invariant manifolds of equilibria and ... See full document
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