Stability Analysis of a Tethered Aerostat
This paper presents a dynamics analysis of a streamlined aerostat tethered to the ground by a single tether. A nonlinear dynamics model of this system is first assembled. The tether is modeled using a lumped mass approach, and the viscoelastic properties of the tether are included. The aerostat is m...
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Veröffentlicht in: | Journal of aircraft 2003-07, Vol.40 (4), p.705-715 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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Zusammenfassung: | This paper presents a dynamics analysis of a streamlined aerostat tethered to the ground by a single tether. A nonlinear dynamics model of this system is first assembled. The tether is modeled using a lumped mass approach, and the viscoelastic properties of the tether are included. The aerostat is modeled using a component breakdown approach. The dynamics equations of the cable and aerostat are then assembled into a single system of nonlinear differential equations. A linearization of this system is then performed using a finite difference approach. The resulting linear equations of motions are decoupled into longitudinal and lateral subsets. The stability properties of each subset is then studied as a function of wind speed. The effect of varying tether length is also investigated. [PUBLICATION ABSTRACT] |
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ISSN: | 0021-8669 1533-3868 |
DOI: | 10.2514/2.3149 |