公开(公告)号：KR101762510B1

公开(公告)日：2017-07-27

申请号：KR1020150149673

申请日：2015-10-27

Applicant: 국방과학연구소

Inventor： 최준성 ,  이정규 ,  김성철

IPC: H04W64/00 ,  H04W84/18 ,  G01S5/14

Abstract: 본발명은위치추정기술에관한것으로서, 더상세하게는생체모방로봇, 감시정찰로봇등 움직일수 있으며자신의위치의정보를서로전달할수 있는통신시스템을갖춘기준노드(RN; Reference Node)를기반으로타겟노드(TN: Target Node)의위치를정확히추정하는동형기준노드위치결정방법에대한것이다.

公开(公告)号：KR1020130122373A

公开(公告)日：2013-11-07

申请号：KR1020120045649

申请日：2012-04-30

Applicant: 국방과학연구소

Inventor： 유천종 ,  김성철 ,  김상호

IPC: G01P21/00 ,  G01F25/00 ,  G01M9/00

CPC classification number: G01P21/025 ,  G01F1/712 ,  G01F25/0084 ,  G01M9/062

Abstract: Provided is an apparatus for calibrating and testing a Mach probe comprising: a front part for installing the Mach probe thereon, facing the wind and forming one end with a wedge type; an installation part connected to the front part for forming a rear part extended to one direction; a supporting rod for supporting the installation part by being extended to one direction and changing an angle of the installation part with respect to the wind; and an installation adaptor for attachably or detachably installing the installation part to the supporting rod. The present invention minimizes an aerodynamic interference imposed on the installation part by the shape of the installation part and adjustment of the installation part angle with the supporting rod, and improves the accuracy of calculating a calibration coefficient of the Mach probe by solving differences of Mach numbers at local areas.

Abstract translation: 提供了一种用于校准和测试马赫探针的装置，包括：前部，用于在其上安装马赫探针，面向风并形成楔形一端; 连接到前部的安装部，用于形成向一个方向延伸的后部; 支撑杆，其通过向一个方向延伸并且相对于风改变安装部的角度来支撑安装部; 以及用于将安装部件可安装或可拆卸地安装到支撑杆的安装适配器。 本发明通过安装部件的形状和与支撑杆的安装部分角度的调整来最小化施加在安装部件上的空气动力学干扰，并且通过求解马赫数的差异来提高计算马赫探针的校准系数的精度 在当地。

公开(公告)号：KR1020130122372A

公开(公告)日：2013-11-07

申请号：KR1020120045647

申请日：2012-04-30

Applicant: 국방과학연구소

Inventor： 유천종 ,  김성철 ,  이종건

IPC: G01M9/06 ,  G01M9/00

Abstract: The present invention provides a flight vehicle model including a deformation preventing unit installed on a support rod which is connected to a balance inside the body of the flight vehicle. The deformation prevention unit touches the inner surface of the body of the flight vehicle in case of the deformation of the balance, thereby preventing the overload of the balance. Therefore, the present invention prevents damage to the balance, which is proper to the size of the flight vehicle model, caused by the overload.

Abstract translation: 本发明提供了一种飞行器模型，其包括安装在支撑杆上的变形防止单元，该变形防止单元连接到飞行器车身内部的平衡体。 变形防止单元在天平变形的情况下接触飞行器体的内表面，从而防止平衡过载。 因此，本发明能够防止由过载引起的对飞行模型的尺寸的适当的平衡的损坏。