[PDF] Top 20 Static highly elliptical orbits using hybrid low-thrust propulsion
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Static highly elliptical orbits using hybrid low-thrust propulsion
... maximum thrust of the solar electric propulsion thruster constrains the ...electric propulsion system is ...maximum thrust, the increase in mission lifetime is greater than that achieved ... See full document
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Static highly elliptical orbits using hybrid low-thrust propulsion
... Observations from GEO begin to degrade at around 55deg latitude; the previous analysis therefore details the minimum requirements to provide continuous global observation at any time. Therefore, to provide a more ... See full document
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Static highly elliptical orbits using hybrid low-thrust propulsion
... maximum thrust of the solar electric propulsion thruster constrains the ...electric propulsion system is ...maximum thrust, the increase in mission lifetime is greater than that achieved ... See full document
35
Survey of highly non-Keplerian orbits with low-thrust propulsion
... of highly non- Keplerian orbits from the larger sets of non-Keplerian orbits (NKOs) and natural Keplerian orbits is ...such orbits is given, tracing the field from its roots to current ... See full document
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Extension of earth orbits using low-thrust propulsion
... of highly elliptical orbit, with a period, typically, of one half of a sidereal day, characteristic of the Molniya orbit is the fixed ...of low-thrust to change the critical inclination of the ... See full document
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Displaced periodic orbits with low-thrust propulsion
... craft propulsion. These propulsion systems can enable exciting new space-science mission concepts such as solar system exploration and deep space ...of highly non-Keplerian or- bits, within the frame ... See full document
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Extension of Martian orbits using continuous low-thrust propulsion
... novel orbits around Mars using continuous low-thrust propulsion to enable new and unique investigations of the red ...acceleration, using Solar Electric Propulsion, to ... See full document
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Designing displaced lunar orbits using low-thrust propulsion
... a static state feedback control u = (X , ν), such that the new control input ν satisfy a linear time-invariant relation Z ˙ = AZ + Bν where the pair (A, B) is ...the hybrid solar sail in the CRTBP is ... See full document
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Low-thrust enabled highly non-Keplerian orbits in support of future Mars exploration
... sail low thrust propulsion systems have their own advantages and ...continuous low thrust indefinitely, although in practice, long-term degradation of the optical surface may reduce the ... See full document
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Novel orbits of Mercury and Venus enabled using low-thrust propulsion
... novel orbits of both Mercury and Venus to enhance the opportunities for remote ...Continuous low-thrust propulsion is used to extend the critical inclination of highly elliptical ... See full document
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Novel orbits of Mercury, Venus and Mars enabled using low-thrust propulsion
... Continuous low-thrust propulsion has been shown to extend highly-elliptical orbits at the critical inclination at Mars, Mercury and Venus, which at Mercury and Mars can be ... See full document
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Artificial three-body equilibria for hybrid low-thrust propulsion
... the elliptical restricted three-body problem and find equilibrium points exist only within the ecliptic ...periodic orbits around these AEPs in and above the ecliptic plane for the solar sail ... See full document
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Hybrid low-thrust transfers to eight-shaped orbits for polar observation
... from low Earth orbit (LEO) to so-called eight-shaped orbits at the collinear libration points in the circular restricted three-body problem are ...these orbits (both natural and sail displaced) for ... See full document
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Extension of the Molniya orbit using low-thrust propulsion
... orbit using low-thrust propulsion is ...proposed, highly elliptical orbits are enabled by existing low-thrust propulsion technology, enabling new ... See full document
20
Displaced geostationary orbits using hybrid low-thrust propulsion
... Electric Propulsion (SEP) has also been considered as a means to maintain displaced NKOs [9, ...is highly efficient as it enables high specific ...a low AD 2 ...of hybrid sails, a ... See full document
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Design of optimal Earth pole-sitter transfers using low-thrust propulsion
... pole-sitter orbits and their control has only recently been performed by Ceriotti et ...electric propulsion (SEP) it was shown that a five year pole-sitter mission with a 100 kg payload ...the ... See full document
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Sun-synchronous highly elliptical orbits using low-thrust propulsion
... UE to restrictions within the current architecture of the global observing system (GOS), space-based remote sensing of Earth suffers from an acute data-deficit over the critical polar-regions. Currently, observation of ... See full document
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Displaced geostationary orbits using hybrid low-thrust propulsion
... spacecraft propulsion system to maintain displaced NKOs [2, 4, 7- 8, ...large, highly reflecting sail to produce a continuous, propellant-less thrust ...primary propulsion system on a ... See full document
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Extension of highly elliptical Earth orbits using continuous low-thrust propulsion
... when low-thrust normal to the orbit plane is included, meaning it is no longer possible to obtain a general perturbations ...combining low-thrust in all three axial directions in-order to ... See full document
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Optimised GTO-GEO transfer using low-thrust propulsion
... uses a direct optimisation method to solve the GTO-GEO trans- fer. The weights to three optimal feedback control laws (for the variation of semimajor axis, eccentricity and inclination) are obtained as solution of a ... See full document
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