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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/65285

    Title: Asymmetrical Chattering Arc in Vertical Plane Flight
    Authors: Chern, Jeng-shing;Chen, Yen-hsun;Hong, Zuu-chang
    Contributors: 淡江大學機械與機電工程學系
    Date: 2000-04
    Issue Date: 2013-05-30 15:25:33 (UTC+8)
    Publisher: Kidlington: Pergamon
    Abstract: The asymmetrical chattering arc of a winged space vehicle in the vertical plane reentry flight has been studied. With the use of dimensionless variables, we need only two parameters to specify the aerodynamic characteristics of the vehicle, one is the ballistic coefficient and the other is the maximum lift-to-drag ratio. The control variable is the normalized lift coefficient (NLC), the ratio of the lift coefficient and the lift coefficient at the maximum lift-to-drag ratio. The chattering flight happens when the NLC switches rapidly between its maximum and minimum values. We use the chattering control on the NLC to obtain maximum drag, or say, maximum deceleration. The asymmetrical chattering arc will be existing when the maximum and minimum NLCs have different absolute values. We started the study of the asymmetrical chattering from an example of basic dynamical system. It is found that a singular arc can be replaced by either a symmetrical or an asymmetrical chattering arc. The net effects on the lift and drag will be the weighted sums of the first and second orders of the maximum and minimum NLCs, respectively. The weighting factor is the percentage of acting time. A typical asymmetrical chattering reentry flight has the characteristics of maximum deceleration and phugoid oscillation.
    Relation: Acta Astronautica 46(7), pp.441-448
    DOI: 10.1016/S0094-5765(99)00187-3
    Appears in Collections:[機械與機電工程學系暨研究所] 期刊論文

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