APPARATUS AND METHOD FOR DETERMINING ORBIT OF GEOSTATIONARY SATELLITE
    1.
    发明申请
    APPARATUS AND METHOD FOR DETERMINING ORBIT OF GEOSTATIONARY SATELLITE 有权
    用于确定地球卫星轨道的装置和方法

    公开(公告)号:US20140055299A1

    公开(公告)日:2014-02-27

    申请号:US13829662

    申请日:2013-03-14

    CPC classification number: G01S19/42 G01S19/14

    Abstract: An apparatus and method for determining an orbit of a geostationary satellite is provided. The orbit of the geostationary satellite may be determined using at least one pseudo-range of the geostationary satellite calculated based on an orbit and a position of at least one global positioning system (GPS) satellite, position information of the geostationary satellite, and an angle between the geostationary satellite and each GPS satellite.

    Abstract translation: 提供了一种用于确定对地静止卫星轨道的装置和方法。 可以使用基于轨道计算的地球静止卫星的至少一个伪距离和至少一个全球定位系统(GPS)卫星的位置,对地静止卫星的位置信息和角度的角度来确定对地静止卫星的轨道 地球静止卫星与每颗GPS卫星之间。

    SPACE OBJECT DISPOSAL DEVICE AND SPACE OBJECT DISPOSAL METHOD
    2.
    发明申请
    SPACE OBJECT DISPOSAL DEVICE AND SPACE OBJECT DISPOSAL METHOD 有权
    空间对象处理设备和空间对象处理方法

    公开(公告)号:US20150251777A1

    公开(公告)日:2015-09-10

    申请号:US14617129

    申请日:2015-02-09

    CPC classification number: B64G1/242

    Abstract: Disclosed are a space object disposal device and a space object disposal method using a rotation motion. The device for disposing a space object includes: a disposal orbit calculation unit configured to calculate a disposal orbit of a space object; an escape velocity calculation unit configured to calculate an escape velocity at which the space object moves along the disposal orbit; and a rotation driving unit configured to be connected the space object, rotate the space object on a predetermined rotation orbit so as to reach the escape velocity, and separate the space object at a point of contact of the predetermined rotation orbit and the disposal orbit when the space object rotates at the escape velocity.

    Abstract translation: 公开了使用旋转运动的空间物体处理装置和空间物体处理方法。 用于设置空间物体的装置包括:废弃轨道计算单元,被配置为计算空间物体的废弃轨道; 逃逸速度计算单元,被配置为计算空间物体沿着处置轨道移动的逃逸速度; 以及旋转驱动单元,被配置为连接所述空间物体,在预定的旋转轨道上旋转所述空间物体以达到所述逃逸速度,并且在所述预定旋转轨道和所述处置轨道的接触点处分离所述空间物体, 空间物体以逃逸速度旋转。

    APPARATUS AND METHOD FOR CONTROLLING GEOSTATIONARY ORBIT SATELLITE
    4.
    发明申请
    APPARATUS AND METHOD FOR CONTROLLING GEOSTATIONARY ORBIT SATELLITE 有权
    用于控制地球轨道卫星的装置和方法

    公开(公告)号:US20130327893A1

    公开(公告)日:2013-12-12

    申请号:US13913005

    申请日:2013-06-07

    CPC classification number: B64G1/242 B64G1/007 B64G1/1007 B64G1/24 B64G1/52

    Abstract: An apparatus and method for controlling a geostationary orbit satellite is provided. The method including generating remote measurement data by measuring a state of a geostationary orbit satellite, transmitting the remote measurement data, receiving a remote command signal, and controlling an orbit and a pose of the geostationary orbit satellite relative to inclined geosynchronous space debris.

    Abstract translation: 提供了一种用于控制地球静止轨道卫星的装置和方法。 该方法包括通过测量对地静止轨道卫星的状态,发送远程测量数据,接收远程命令信号,以及相对于倾斜的地球同步空间碎片控制对地静止轨道卫星的轨道和姿态来产生远程测量数据。

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