1985
DOI: 10.2514/3.45189
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Generalized math model for simulation of high-altitude balloon systems

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Cited by 12 publications
(12 citation statements)
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“…Table 1 presents the frequencies of the eigenmodes predicted by the proposed model, i.e. the solutions in ω of the characteristic equation det(Mω 2 − K) = 0 where M and K are defined by equations (18) and (19), respectively.…”
Section: Application Of the Modeling Methods And Comparison With Flight Datamentioning
confidence: 99%
See 2 more Smart Citations
“…Table 1 presents the frequencies of the eigenmodes predicted by the proposed model, i.e. the solutions in ω of the characteristic equation det(Mω 2 − K) = 0 where M and K are defined by equations (18) and (19), respectively.…”
Section: Application Of the Modeling Methods And Comparison With Flight Datamentioning
confidence: 99%
“…The pendulum modes 3 and 4 represented a large contribution to the telescope's pointing error during the FIREBall 2018 flight [3]. Modes 3 and 4 can be excited by wind gusts [18], but also by the azimuth control of the gondola because of the inertia coupling. Pendulum modes of higher frequency (5 and more) are essentially oscillations of the elements of the flight train.…”
Section: Application Of the Modeling Methods And Comparison With Flight Datamentioning
confidence: 99%
See 1 more Smart Citation
“…zodiacal light or airglow) with wide field of view (FOV) instruments. A key requirement for these observations is accurate and stable pointing in spite of the wind speeds of tens of knots and local turbulence known to exist at altitudes above 30 km [Chingcuanco, 1989], which cause the payload to sway and rotate [Hazen, 1985;Nigro et al, 1985]. We are developing a 3-axis stabilization system to correct for these random motions, where the first step is development of an attitude sensor to determine the pointing direction.…”
Section: Introductionmentioning
confidence: 99%
“…With wider applications of high-altitude balloons as a cost-effective means in the Earth's atmosphere, there is growing interest in assessing balloon performance and failure mechanism. 1 Various experimental [2][3][4] and analytical 2,5,6 techniques have been developed to predict geometrical shape and stress state of high-altitude balloon. Most of experimental methods are still largely based on experience and empirical data for balloon analysis.…”
Section: Introductionmentioning
confidence: 99%