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[PDF] Top 20 Solar Sail Equilibrium Orbits in the Circular Restricted Three Body Problem with Oblateness

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Solar Sail Equilibrium Orbits in the Circular Restricted Three Body Problem with Oblateness

Solar Sail Equilibrium Orbits in the Circular Restricted Three Body Problem with Oblateness

... The restricted three-body problem with the larger primary a source of radiation and the smaller primary an ob- late spheroid is ...the circular restricted ... See full document

10

Lissajous Orbits at the Collinear Libration Points in the Restricted Three Body Problem with Oblateness

Lissajous Orbits at the Collinear Libration Points in the Restricted Three Body Problem with Oblateness

... Using a barycentric-synodic coordinate system ( ξ η ζ , , ) and dimensionless variables, the equations of motion of a test particle in the circular restricted three-body problem under ... See full document

11

Triangular Libration Points in Elliptic Photogravitational Restricted Three Body Problem with Oblateness

Triangular Libration Points in Elliptic Photogravitational Restricted Three Body Problem with Oblateness

... elliptic restricted three-body problem (ER3BP) describes the three-dimensional motion of a small particle, called the third body (infinitesimal mass) under the gravitational ... See full document

6

Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits

Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits

... a solar sail in the Earth-Sun circu- lar restricted 3-body ...the sail are given by a set of nonlinear autonomous ordinary differential equations, which are non-conservative due to the ... See full document

13

Stabilization of displaced periodic orbits in the solar sail restricted three-body system

Stabilization of displaced periodic orbits in the solar sail restricted three-body system

... Outline Solar Sails • Sail Design - Practical Goal Earth-Moon Restricted Three-Body Problem • System Model - Equations of Motion of the Hybrid Sail • Linearized System • Conditions for t[r] ... See full document

53

Extension of Earth-Moon libration point orbits with solar sail propulsion

Extension of Earth-Moon libration point orbits with solar sail propulsion

... classical circular restricted three-body problem with a solar ...the solar sail induced acceleration, families of Lyapunov, halo, ver- tical Lyapunov, ... See full document

20

Solar sail equilibria in the elliptical restricted three-body problem

Solar sail equilibria in the elliptical restricted three-body problem

... the solar sail elliptical restricted three-body problem, and the following results obtained: There are no equilibrium surfaces in the three-dimensional, elliptical ... See full document

27

Halo Orbits in the Photo Gravitational Restricted Three Body Problem

Halo Orbits in the Photo Gravitational Restricted Three Body Problem

... The circular restricted three-body problem (CRTBP) is a special case of the restricted three-body problem where bigger and smaller primaries move in cir- ... See full document

18

Halo Orbits around Sun Earth L1 in Photogravitational Restricted Three Body Problem with Oblateness of Smaller Primary

Halo Orbits around Sun Earth L1 in Photogravitational Restricted Three Body Problem with Oblateness of Smaller Primary

... the restricted three-body problem are relatively less accurate for studying the motion of any Sun-planet system as they do not account for the effect of the perturbing forces such as ... See full document

19

Displaced periodic orbits with low-thrust propulsion

Displaced periodic orbits with low-thrust propulsion

... and solar electric technology provide alternative forms of space- craft ...as solar system exploration and deep space ...Earth-Moon circular restricted three-body problem ... See full document

15

Stabilizing periodic orbits above the elliptic plane in the solar sail 3-body problem

Stabilizing periodic orbits above the elliptic plane in the solar sail 3-body problem

... no equilibrium points in this ...periodic orbits above the ecliptic ...the circular case (e = 0) ...the solar sail to track using variations in its ...term’ solar sail is ... See full document

7

Existence and Stability of Equilibrium Points in the Robe’s Restricted Three Body Problem with Variable Masses

Existence and Stability of Equilibrium Points in the Robe’s Restricted Three Body Problem with Variable Masses

... The restricted three-body problem (R3BP) describes the motion of an infinitesimal mass moving under the gravi- tational effects of the two finite masses, called primaries, which move in ... See full document

10

Invariant manifolds and orbit control in the solar sail three-body problem

Invariant manifolds and orbit control in the solar sail three-body problem

... of solar sails in the circular restricted Earth-Sun ...for solar sails in this system have the linear dynamical properties of saddles crossed with centers; thus the fixed points are ... See full document

15

Solar Radiation Pressure Effects on Stability of Periodic Orbits in Restricted Four Body Problem

Solar Radiation Pressure Effects on Stability of Periodic Orbits in Restricted Four Body Problem

... Periodic orbits in the photo gravitational restricted problem when the primaries are tri-axial rigid bodies were investigated ...of Solar Radiation Pressure on the Libration Points of the ... See full document

14

Feedback stabilization of displaced periodic orbits : applications to binary asteroids

Feedback stabilization of displaced periodic orbits : applications to binary asteroids

... 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

16

Feedback stabilization of displaced periodic orbits : Application to binary asteroid

Feedback stabilization of displaced periodic orbits : Application to binary asteroid

... periodic orbits at linear order in the circular re- stricted Earth-Moon system (CRTBP), where the third massless body utilizes a hybrid of solar sail and a solar electric ... See full document

17

Solar sail Lyapunov and halo orbits in the Earth-Moon three-body problem

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 further ... See full document

18

Solar sail orbits at the Earth-Moon libration points

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

New periodic orbits in the solar sail restricted three body problem

... the sail angles γ and φ, and solving F = ...for orbits we initially assume φ = 0 so the equilibrium (and sail normal) is in the x-z ... See full document

11

On the Artificial Equilibrium Points in a Generalized Restricted Problem of Three Bodies

On the Artificial Equilibrium Points in a Generalized Restricted Problem of Three Bodies

... electric sail was proposed to be designed which could be capable of guarantying the fulfillment of trajectories that would be otherwise unfeasible through conventional ...electric sail capabilities of ... See full document

9

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