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Optimal steering law for the GeoSail mission

Mengali, G, Quarta, AA and Lappas, VJ (2007) Optimal steering law for the GeoSail mission Journal of Guidance, Control, and Dynamics, 30 (3). pp. 876-879.

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Abstract

An optimal steering law has been developed for meeting the requirements of maximizing the apse-line precession capability and the solar rotation required to attain a precession rate for GeoSail mission. The steering law takes into account all of the fundamental effects influencing the sail performance capabilities, including the shadowing effects due to the eclipse periods. A linear relationship obtained between the solar sail characteristic acceleration and the apse-line precession rate, allow evaluation of solar sail acceleration, ae necessary to perform the mission. The value of solar sail acceleration can be increased by a safety margin to compensate for the optical characteristic degradation of the sail due to a long residence in a hostile environment. The optimal steering law provide significant performance improvement with respect to simply orienting, at all time, the solar sail panel to the sun-sail line.

Item Type: Article
Authors :
NameEmailORCID
Mengali, GUNSPECIFIEDUNSPECIFIED
Quarta, AAUNSPECIFIEDUNSPECIFIED
Lappas, VJv.lappas@surrey.ac.ukUNSPECIFIED
Date : 1 May 2007
Identification Number : https://doi.org/10.2514/1.28765
Depositing User : Symplectic Elements
Date Deposited : 17 May 2017 11:25
Last Modified : 17 May 2017 11:25
URI: http://epubs.surrey.ac.uk/id/eprint/831307

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