This article discusses the maintenance of an L-1-type artificial equilibrium point in the Sun-[Earth+Moon] circular restricted three-body problem by means of an electric solar wind sail. The reference configuration instability is compensated for with a feedback control law that adjusts the grid voltage as a function of the distance from the natural L-1 point. Two different control strategies are analyzed assuming the solar wind fluctuations to be modeled through a statistical approach.
Artificial Collinear Lagrangian Point Maintenance With Electric Solar Wind Sail
Niccolai LPrimo
Software
;Caruso ASecondo
Validation
;Quarta A
Penultimo
Conceptualization
;Mengali GUltimo
Formal Analysis
2020-01-01
Abstract
This article discusses the maintenance of an L-1-type artificial equilibrium point in the Sun-[Earth+Moon] circular restricted three-body problem by means of an electric solar wind sail. The reference configuration instability is compensated for with a feedback control law that adjusts the grid voltage as a function of the distance from the natural L-1 point. Two different control strategies are analyzed assuming the solar wind fluctuations to be modeled through a statistical approach.File in questo prodotto:
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[2020] Artificial Collinear Lagrangian Point Maintenance with Electric Solar Wind Sail.pdf
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TAES_v56_n6_2020.pdf
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