Surfing the L2 gradient with the starshade in search of extraterrestrial life

Conference Paper (2016)
Author(s)

CMA Deccia (University of Colorado)

Eduardo Villalba (University of Colorado)

JS Parker (University of Colorado)

GH Born (University of Colorado)

Webster Cash (University of Colorado)

R Noomen (TU Delft - Astrodynamics & Space Missions)

Research Group
Astrodynamics & Space Missions
DOI related publication
https://doi.org/10.2514/6.2016-5666
More Info
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Publication Year
2016
Language
English
Research Group
Astrodynamics & Space Missions
ISBN (electronic)
978-1-62410-445-9

Abstract

A heliogyro is a solar sail concept that divides the solar sail membrane into a number of long, slender blades of film extended from a central hub, maintained in a flat state through spin-induced tension. The heliogyro can redirect and scale the solar radiation pressure (SRP) force and can achieve attitude control by twisting the blades, similar to a helicopter rotor. Different pitch profiles exist, including pitching the blades in a collective, cyclic or combined collective and cyclic manner. While the forward mapping, i.e., computing the SRP force and moment generated by the heliogyro for a given pitch profile, is straightforward, the inverse of the problem is much more complex. However, this inverse problem (finding the blades’ pitch that results in a desired SRP force and/or moment) is crucial for heliogyro mission design and operations. This paper therefore solves the inverse problem numerically: first, only for a desired SRP force or SRP moment and subsequently for the fully coupled inverse problem. The developed methods are subsequently applied to track a reference trajectory that corrects for injection errors into a solar sail Sun-Earth sub-L1 halo orbit.
I. Introduction

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