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elliptical orbit

EQUILIBRIUM POSITIONS OF A CABLE-CONNECTED SATELLITES SYSTEM UNDER THE INFLUENCE OF SOLAR RADIATION PRESSURE, EARTH'S SHADOW, EARTH'S OBLATENESS AND AIR RESISTANCE: ELLIPTICAL ORBIT

EQUILIBRIUM POSITIONS OF A CABLE-CONNECTED SATELLITES SYSTEM UNDER THE INFLUENCE OF SOLAR RADIATION PRESSURE, EARTH'S SHADOW, EARTH'S OBLATENESS AND AIR RESISTANCE: ELLIPTICAL ORBIT

... We study the equilibrium positions of the motion of a system of two cable-connected artificial satellites under the influence of solar radiation pressure, earth's oblateness, shadow of the earth and air resistance. The ...

7

A CABLE-CONNECTED SATELLITES SYSTEM UNDER SEVERAL INFLUENCES OF GENERAL NATURE AND ELLIPTICAL ORBIT

A CABLE-CONNECTED SATELLITES SYSTEM UNDER SEVERAL INFLUENCES OF GENERAL NATURE AND ELLIPTICAL ORBIT

... We derive a set of non-linear, non-homogeneous and non-autonomous differential equations for the motion of a system of two cable-connected artificial satellites under the influence of shadow of the earth, solar radiation ...

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Effects of a Time Varying Moment on a Large Tethered Satellite in Circular or Elliptical Orbit

Effects of a Time Varying Moment on a Large Tethered Satellite in Circular or Elliptical Orbit

... The purpose of this paper is to investigate the effect of a varying moment on the rotation angle of a large tethered satellite that is orbiting a planet. Two different types of orbits were investigated: a simple circular ...

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End-of-life disposal trajectories for libration point and highly elliptical orbit missions

End-of-life disposal trajectories for libration point and highly elliptical orbit missions

... A differential correction procedure is implemented to match in position the actual LPO to the unstable invariant manifold of the LPO computed from the initial conditions in Table 2. The ac- tual initial condition for the ...

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End-of-life disposal concepts for libration point and highly elliptical orbit missions

End-of-life disposal concepts for libration point and highly elliptical orbit missions

... graveyard orbit for HEOs, while spacecraft on LPOs can be disposed through an Earth re-entry, or can be injected onto trajectories towards a Moon impact, or towards the inner or the outer solar system, by means of ...

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End-of-life disposal concepts for libration point orbit and highly elliptical orbit missions

End-of-life disposal concepts for libration point orbit and highly elliptical orbit missions

... Libration Point Orbits (LPOs) and Highly Elliptical Orbits (HEOs) are often se- lected for astrophysics and solar terrestrial missions. No guidelines currently ex- ist for their end-of life. However, as current ...

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High Accuracy Relative Motion of Spacecraft Using Linearized Time-Varying J2-Perturbed Terms

High Accuracy Relative Motion of Spacecraft Using Linearized Time-Varying J2-Perturbed Terms

... reference orbit, of an object in an inverse square gravity ...an elliptical orbit, but they had to regularize the problem, resulting in a solution that does not explicitly include ...

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Time-delayed feedback control in astrodynamics

Time-delayed feedback control in astrodynamics

... periodic orbit about a body with large ellipticity (such as an asteroid) and finally, we apply TDFC to eliminate the drift between two satellites in low Earth orbits to ensure their relative motion is ...

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Orbits in a generalized two-body problem

Orbits in a generalized two-body problem

... transfer orbit apriori, other approaches can also be ...an elliptical orbit can be sought that connects the initial and Ž nal circular orbits in a quasi-Hohmann ...circular orbit radii r O and ...

8

Selection of an orbit for communication satellite based on inclination and eccentricity

Selection of an orbit for communication satellite based on inclination and eccentricity

... Transfer Orbit (GTO): It is an elliptical orbit of the ...transfer orbit which helps the launch vehicle to launch its payload form LEO to ...

5

Enhancing Rollover Threshold of an Elliptical Container Based on Binary-coded Genetic Algorithm

Enhancing Rollover Threshold of an Elliptical Container Based on Binary-coded Genetic Algorithm

... The circular cross-section has a high center of mass location, but considerably less lateral load transfer with low fill volumes under a steady turning lateral acceleration field. On the other hand, modified oval tanks ...

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DECODING OF ORBIT CODES

DECODING OF ORBIT CODES

... explains syndrome decoding of irreducible cyclic orbit codes. The main idea is that the pairwise quotients of the elements of a subspace are invariant for all elements of the same orbit. When the number of ...

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Effects Analysis of Frozen Conditions for Spacecraft Relative Motion Dynamics

Effects Analysis of Frozen Conditions for Spacecraft Relative Motion Dynamics

... the orbit, depending on the orientation of the ...frozen orbit as the reference orbit of the ...LEO orbit [5]. Basis researches show that the eccentricity frozen orbit was first ...

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Birefringence analysis of segmented cladding fiber

Birefringence analysis of segmented cladding fiber

... The radial effective index method (REIM) has been conventionally used to determine the propagation characteristics in terms of effective index and leak- age loss of the modes of an SCF. However, REIM, being a scalar ...

6

The Elliptical Lead Zeppelin

The Elliptical Lead Zeppelin

... All the components are built, only the switch needs to be made to work. If this is done, one could most likely start to measure immediately. After this, we can look if the theoretical and numerical predictions are ...

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Data Driven Nonlinear Control for Orbit Transfer: From the Earth to Moon and L4/5

Data Driven Nonlinear Control for Orbit Transfer: From the Earth to Moon and L4/5

... change orbit from the earth to the moon. During the orbit change, the zero velocity curve serves as a indication of the potential energy level that the satellite must process to travel ...

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Orbit Closures and Invariants

Orbit Closures and Invariants

... AG.10.3], e(v) is an upper semi-continuous function of v. This implies the following use- ful result about dimensions of stabilizers for a G-variety X [44, Lemma 3.7(c)]: for any r ∈ N ∪ {0}, the set {x ∈ X | dim(G x ) ≥ ...

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A meteor orbit radar

A meteor orbit radar

... The time of occurrence, range, duration of the trail, three echo amplitude profiles and two phase angle profiles are recorded for each meteor observation.. From this information the rela[r] ...

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J-integral analysis of a sub-clad crack under PTS transient

J-integral analysis of a sub-clad crack under PTS transient

... In this work, a subsurface crack near the surface is characterized to be 3 different models, including surface crack, subclad semi-elliptical crack, and embed elliptical crack. The fracture mechanics ...

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Multi-objective optimisation of constellation deployment using low-thrust propulsion

Multi-objective optimisation of constellation deployment using low-thrust propulsion

... in orbit around the Earth increases it is also paramount to devise an appropri- ate de-orbiting strategy for the spacecraft at the end of the constellation ...

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