The invention relates to a processing method for aircraft control surface rotational inertia coordinate transformation, and belongs to the field of aircraft weight engineering. The aircraft control surface rotational inertia coordinate transformation method comprises the following steps: (1) simplifying the relationship between a rotating shaft and an original aircraft coordinate system, randomlytaking two points on the rotating shaft, solving the projection length of a straight line segment between the two points and each coordinate system based on the three-dimensional coordinate values ofthe two points, and further solving the included angle between the straight line segment and each projection; (2) constructing a relational graph between gravity center points and a rotating shaft, and calculating a spatial distance from the control surface gravity center to the rotating shaft axis; and (3) inputting the weight, gravity center and rotational inertia parameters of the control surface under the airplane coordinate system, and coordinate values of two points on the axis to be converted, so as to calculate the rotational inertia around the rotating shaft. The method has the advantages that the trigonometric function is calculated to replace a drawing method, and the problems that three-dimensional space drawing is difficult to interpret and errors are prone to occurring are solved.

    本发明涉及一种飞机舵面转动惯量坐标变换的处理方法,属于飞机重量工程领域。一种飞机舵面转动惯量坐标变换方法,包括以下步骤:(1)简化转轴与原飞机坐标系的关系,在转轴上任意取两个点,基于两点三维坐标值,求得两点间直线段与各坐标系的投影长度,进而求得直线段与各投影的夹角;(2)构建重心点距转轴的关系图,计算舵面重心至转轴轴线的空间距离;(3)输入舵面在飞机坐标系下的重量、重心和转动惯量参数,以及所需转化的轴线上两个点坐标值,即可计算出绕转轴的转动惯量。本发明具有如下优点:用计算三角函数来代替作图法,解决了三维空间作图难以判读并容易出错的问题。


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    Titel :

    Aircraft control surface rotational inertia coordinate transformation method


    Weitere Titelangaben:

    一种飞机舵面转动惯量坐标变换方法


    Beteiligte:
    HUANG WEI (Autor:in) / LIN ZIPING (Autor:in) / ZHONG XIJIAN (Autor:in) / ZHANG JING (Autor:in) / ZANG ZIHAO (Autor:in) / LU SEN (Autor:in)

    Erscheinungsdatum :

    02.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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