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low Earth orbit spacecraft

Design of ballistic three-body trajectories for continuous polar Earth observation in the Earth-Moon system

Design of ballistic three-body trajectories for continuous polar Earth observation in the Earth-Moon system

... polar Earth observation in the Earth-Moon ...polar-orbiting spacecraft, which offer high resolution imaging but poor temporal resolution, due to the fact that they can only capture one narrow swath ...

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An Assessment of Rare Earth Aluminates as Possible Radiation Shields for Artificial Satellites in Low Earth Orbit

An Assessment of Rare Earth Aluminates as Possible Radiation Shields for Artificial Satellites in Low Earth Orbit

... [2] Iucci, N., Dorman, L.I., Levitin, A.E., Belov, A.V., Eroshenko, E.A., Ptitsyna, N.G., Villoresi, G., Chizhenkov, G.V., Gromova, L.I., Parisi, M., Tyasto, M.I. and Yanke, V.G. (2006) Spacecraft Operational ...

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Novel numerical optimisation of the Hohmann Spiral Transfer

Novel numerical optimisation of the Hohmann Spiral Transfer

... and Earth- ...working orbit is ...novel orbit transfer, recently introduced by the authors through an analytical analysis, known as the Hohmann Spiral Transfer ...and low-thrust ...the ...

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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

... require low delta-v ...the spacecraft maintains a 1:1 resonance with the Earth and may return in several ...current spacecraft, but could be implemented on future spacecraft as it is a ...

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Earth’s Magnetic Field for Spacecraft Attitude Control Applications (TECHNICAL NOTE)

Earth’s Magnetic Field for Spacecraft Attitude Control Applications (TECHNICAL NOTE)

... in low earth orbit (LEO) has an increasing ...of spacecraft by the interaction between the earth’s magnetic field and the magnetic dipoles generated in the satellite ...

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Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems

Orbit period modulation for relative motion using continuous low thrust in the two-body and restricted three-body problems

... small, low-cost ...circular orbit of arbitrary dimension, orientation, and period rela- tive to a target on a circular two-body ...relative orbit in the two-body rotating frame, with potential future ...

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A novel design concept for space-based polar remote sensing

A novel design concept for space-based polar remote sensing

... the Earth is conducted from a fleet of spacecraft in two basic orbital positions, near-polar low-Earth orbits and geosynchronous orbits, with each offering its own advantages and ...

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Automatic trajectory planning for low-thrust active removal mission in Low-Earth Orbit

Automatic trajectory planning for low-thrust active removal mission in Low-Earth Orbit

... into orbit over 10,000 objects (Rossi & Valsecchi, ...manned spacecraft in Earth ...within Low Earth Orbit (LEO) have already reached a critical density of objects which will ...

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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

... require low delta-v ...the spacecraft maintains a 1:1 resonance with the Earth and may return in several ...current spacecraft, but could be implemented on future spacecraft as it is a ...

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Synoptic ozone, cloud reflectivity, and erythemal irradiance from sunrise to sunset for the whole earth as viewed by the DSCOVR spacecraft from the earth–sun Lagrange 1 orbit

Synoptic ozone, cloud reflectivity, and erythemal irradiance from sunrise to sunset for the whole earth as viewed by the DSCOVR spacecraft from the earth–sun Lagrange 1 orbit

... with low earth orbit satel- lite data, a more complete comparison can be made with the assimilated ozone product from MERRA-2, the Modern-Era Retrospective Analysis for Research and Applications ...

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Time-delayed feedback control in astrodynamics

Time-delayed feedback control in astrodynamics

... elliptical orbit. Secondly, we apply TDFC to the problem of maintaining a spacecraft in a periodic orbit about a body with large ellipticity (such as an asteroid) and finally, we apply TDFC to ...

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Automatic planning and scheduling of active removal of non-operational satellites in low earth orbit

Automatic planning and scheduling of active removal of non-operational satellites in low earth orbit

... servicing spacecraft to de-orbit several objects applying two different ...servicing spacecraft rendezvous with multiple objects in order to physically attach a de-orbiting kit that performs the ...

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Solar Arrays and Battery Power Sources Conceptual Design for Low Earth Orbit Microsatellites

Solar Arrays and Battery Power Sources Conceptual Design for Low Earth Orbit Microsatellites

... satellites are required to fulfill their requirements on power consumption to sustain their life in space. As typical ones use photovoltaic cells to generate solar power, the presence of a sunlight phase is important. ...

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Design of trajectories for continuous polar Earth observation in the Earth-Moon system

Design of trajectories for continuous polar Earth observation in the Earth-Moon system

... the Earth-Moon ...a spacecraft with respect to the lunar orbital plane, 11 without the need of expensive thrusting ...the orbit hovers over a pole of the Earth, the second one has a very ...

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Self-organising low Earth orbit constellations for Earth observation

Self-organising low Earth orbit constellations for Earth observation

... in low-cost spacecraft technologies, miniaturisation and mass- production, are widening access to space, and are predicted to give rise to future deployments of much larger satellite constellations than ...

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Remote automated multi generational growth and observation of an animal in low Earth orbit

Remote automated multi generational growth and observation of an animal in low Earth orbit

... the International Space Station (ISS) [9], with the Opti- Cell (BioCrystal, Ltd.), which displayed no undesirable issues with spaceflight hardware [18]. OptiCells were linked together by infusion pump tubing and payload ...

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Atmospheric Remnants in the Low Earth Orbit Region around 200 km Altitude

Atmospheric Remnants in the Low Earth Orbit Region around 200 km Altitude

... quite low pressures, of about 10 −9 Pa at 200 km ...the Earth magnet- ic field most of the charged particles coming from the Sun are deflected, but a considerable fraction of them still enters in the polar ...

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Trajectory Design and Optimization for LEO Satellites in Formation to Observe GEO Satellites’ Beams

Trajectory Design and Optimization for LEO Satellites in Formation to Observe GEO Satellites’ Beams

... The problem is a multi-object optimization problem, which appears in many practical applications. For example, the multi-asteroid exploration, the mul- ti-planet exploration and the multi-debris clearing mission [8] [9]. ...

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The Research of Low Earth Orbit Prediction of Satellite Based on Deep Neural Network

The Research of Low Earth Orbit Prediction of Satellite Based on Deep Neural Network

... satellite orbit prediction, the long short-term memory neural network prediction is carried out based on the actual data of X, Y and Z coordinates of the satellite's geocentric inertial coordinate ...near-circular ...

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Physics 20 - Unit C5.5 Keplers Laws.pptx

Physics 20 - Unit C5.5 Keplers Laws.pptx

... distance from the centre of the Earth to the surface of the Earth, not the size of Earth’s orbit.[r] ...

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