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EnglishThe aim of this Note is to explore the capabilities of the emerging EMP technology for the active stabilization of L1-type AEPs using a square solar sail with a fixed attitude. The problem is addressed within an elliptic restricted framework, which is a more realistic model with respect to the classical circular case [4]. The main spacecraft parameters, including the sail side and the total spacecraft mass, are defined, by means of a simplified mathematical model, as a function of the main mission requirements in terms of maximum allowed sail lightness number variation and AEP position.
| Autori interni: | ALIASI, GENEROSO (Primo) MENGALI, GIOVANNI (Secondo) QUARTA, ALESSANDRO ANTONIO (Ultimo) |
| Autori: | Aliasi, Generoso; Mengali, Giovanni; Quarta, ALESSANDRO ANTONIO |
| Titolo: | Artificial Lagrange Points for Solar Sail with Electrochromic Material Panels |
| Anno del prodotto: | 2013 |
| Abstract: | The aim of this Note is to explore the capabilities of the emerging EMP technology for the active stabilization of L1-type AEPs using a square solar sail with a fixed attitude. The problem is addressed within an elliptic restricted framework, which is a more realistic model with respect to the classical circular case [4]. The main spacecraft parameters, including the sail side and the total spacecraft mass, are defined, by means of a simplified mathematical model, as a function of the main mission requirements in terms of maximum allowed sail lightness number variation and AEP position. |
| Digital Object Identifier (DOI): | 10.2514/1.58167 |
| Appare nelle tipologie: | 1.1 Articolo in rivista |
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