2019
DOI: 10.1016/j.actaastro.2018.12.041
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Downrange manoeuvre and oscillation suppression of a self-regulating centrifugally deployed flexible heat shield using a controlled reaction wheel

Abstract: Downrange manoeuvre and oscillation suppression of a self-regulating centrifugally deployed flexible heat shield using a controlled reaction wheel. Acta Astronautica.

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Cited by 5 publications
(7 citation statements)
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“…For the same reason, a larger heat shield can reach a lower instantaneous deployment angle, leading to a higher aeroelastic oscillation (i.e. oscillation in deployment angle, which is investigated in the previous study [33]), which in turn increases the fluctuation in deceleration.…”
Section: )mentioning
confidence: 81%
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“…For the same reason, a larger heat shield can reach a lower instantaneous deployment angle, leading to a higher aeroelastic oscillation (i.e. oscillation in deployment angle, which is investigated in the previous study [33]), which in turn increases the fluctuation in deceleration.…”
Section: )mentioning
confidence: 81%
“…Based on the design studies performed previously [32,33], the present work demonstrates the scalability of DESCENT, and thereby the possibility to adapt this design to a wide range of aerospace applications. Feasibility of re-entry vehicles with entry mass scaled from 30 g to 30 tonne is discussed based on the entry trajectory and structural dynamic behaviour predicted by simulation.…”
Section: Introductionmentioning
confidence: 85%
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“…Assuming λ i is the pole of the low-frequency oscillation information mode, its relative residue R k can be used as an observable indicator. Calculating |R k | can clarify the change of observable level with the change of different operating modes, and the residue ratio is used as the indicator to weigh the observability of the alternative input signal of the TCSC device [19]. e residue is expressed as…”
Section: Adaptive Configuration Of Low-frequency Electromechanical Sampling Information Based On Tcscmentioning
confidence: 99%