[PDF] Top 20 Solar sail orbits at the Earth-Moon libration points
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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
Displaced solar sail orbits : Dynamics and applications
... use solar sail propulsion to provide station-keeping at periodic orbits about the triangular libration points using small variations in the sail’s ...the sail in the ... See full document
11
Displaced periodic orbits with low-thrust propulsion
... and solar electric technology provide alternative forms of space- craft ...as solar system exploration and deep space ...the Earth-Moon circular restricted three-body problem (CRTBP), where ... See full document
15
Displaced solar sail orbits : dynamics and applications
... use solar sail propulsion to provide station-keeping at periodic orbits about the triangular libration points using small variations in the sail’s ...the sail in the ... See full document
11
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
Optimal solar sail interplanetary heteroclinic transfers for novel space applications
... as libration point orbits, are all unstable. Orbits of family f, originating as retrograde orbits about the smaller primary, are all ...stable. Orbits of families g and g 0 , ... See full document
37
Quantum effects on Lagrangian points and displaced periodic orbits in the Earth-Moon system
... that is, with respect to an appropriately chosen coordinate reference system. One potential choice is the International Terrestrial Reference system (ITRS) [55], which is established with several geodesy techniques, ... See full document
36
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 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
Feedback stabilization of displaced periodic orbits : Application to binary asteroid
... 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 propulsion ... See full document
17
Analysis and control of displaced periodic orbits in the Earth-Moon system
... as solar system exploration and deep space observation. A solar sail is propelled by reflecting solar photons and therefore can transform the momentum of the photons into a propul- sive ... See full document
7
Earth-Moon Lagrangian points as a testbed for general relativity and effective field theories of gravity
... the Earth-Moon ...Lagrangian points is governed by four algebraic ninth degree equations, which reduce to two algebraic fifth degree equations in the classical regime, while the quantum corrected ... See full document
41
Feedback stabilization of displaced periodic orbits : applications to binary asteroids
... 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
16
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
Lissajous Orbits at the Collinear Libration Points in the Restricted Three Body Problem with Oblateness
... equilibrium points of the restricted three-body problem are studied under the effect of oblateness of the bigger primary using an analytical and numerical ...periodic orbits around these points are ... See full document
11
Design and applications of solar sail periodic orbits in the non-autonomous Earth-Moon system
... flower-shaped orbits and other existing and proposed mission concepts for high-latitude Earth observation requires more detailed ...shaped orbits appear to provide a midway between a constellation of ... See full document
20
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 ... See full document
11
Orbital motions of a solar sail around the L2 Earth-Moon libration point
... The solution depends on the SRP acceleration, which is determined by the trigonometric functions of and (time-dependent). It is difficult to derive the explicit solution without any simplification on the expression ... See full document
19
Solar sail trajectories at the Earth-Moon Lagrange points
... periodic orbits above the plane at linear ...suitable sail attitude control program, a 100 km dis- placed, out-of-plane trajectory around the L 4 point ... See full document
7
Extension of Earth-Moon libration point orbits with solar sail propulsion
... classical Earth-Moon circular re- stricted three-body dynamics with a solar sail acceleration, families of solar sail Lyapunov, halo, vertical Lyapunov, Earth-centred and ... See full document
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