Dissertation/Thesis Abstract

Attitude Dynamics, Stability, and Control of a Heliogyro Solar Sail
by Pimienta-Penalver, Adonis Reinier, Ph.D., State University of New York at Buffalo, 2017, 150; 10217274
Abstract (Summary)

A heliogyro solar sail concept, dubbed `HELIOS', is proposed as an alternative to deep space missions without the need for on-board propellant. Although this type of solar sail has existed in concept for several decades, and some previous studies have investigated certain aspects of its operation, a significant amount of research is still needed to analyze the dynamic and control characteristics of the structure under the projected range of orbital conditions. This work presents an improvement upon the existing discrete-mass models of the heliogyro blade, and the extension of its application from a single membrane blade to a fully-coupled approximation of the dynamics of the HELIOS system with multiple spinning membrane blades around a central hub. The incorporation of structural stiffness and external forcing effects into the model is demonstrated to add a further degree of fidelity in simulating the stability properties of the system. Additionally, the approximated dynamics of multiple-blade heliogyro structures are examined under the effect of solar radiation pressure. Lastly, this study evaluates a control algorithm at each blade root to impose structural integrity and attitude control by coordinating well-known helicopter blade pitching profiles.

Indexing (document details)
Advisor: Crassidis, John L.
Commitee: Mook, D. J., Nouh, Mostafa
School: State University of New York at Buffalo
Department: Mechanical and Aerospace Engineering
School Location: United States -- New York
Source: DAI-B 79/02(E), Dissertation Abstracts International
Source Type: DISSERTATION
Subjects: Engineering, Aerospace engineering, Mechanical engineering
Keywords: Gossamer, HELIOS, Heliogyro, Lumped mass, SRP, Solar sail
Publication Number: 10217274
ISBN: 9780355306965
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