公开(公告)号：US07197381B2

公开(公告)日：2007-03-27

申请号：US10728869

申请日：2003-12-08

申请人： Suneel Ismail Sheikh ,  Darryll John Pines ,  Kent S. Wood ,  Paul Shelton Ray ,  Michael N. Lovellette

发明人： Suneel Ismail Sheikh ,  Darryll John Pines ,  Kent S. Wood ,  Paul Shelton Ray ,  Michael N. Lovellette

IPC分类号： G06F7/00 ,  G06F17/00

CPC分类号： B64G1/36

摘要： A system and method for navigation utilizing sources of pulsed celestial radiation are provided. A spacecraft, satellite, or other vehicle (12) has a pulse sensor (22) mounted thereto for detecting signal pulses (14) generated by a plurality of pulsars or other celestial objects (16). The detected signal pulses (14) are synchronously averaged at the known period of the pulsar or other celestial object (16) with respect to a timer (24). Timer (24) measures the pulse time of arrival at the pulse sensor (22) by comparing the pulse signal (14) with a pulse shape template (52), and a processing means (30) calculates the offset time between the measured pulse time of arrival at sensor (22) with a calculated pulse time of arrival at the solar system barycenter (SSBC). The positions and pulse profile characteristics of the pulsars (16) are stored in a digital memory (34) and combining the calculated time offset with the known positions of pulsars (16), the navigational position, velocity, attitude and time of spacecraft (12) with respect to the SSBC can be calculated.

摘要翻译： 提供了利用脉冲天体辐射源的导航系统和方法。 航天器，卫星或其他车辆（12）具有安装在其上的脉冲传感器（22），用于检测由多个脉冲星或其他天体（16）产生的信号脉冲（14）。 所检测的信号脉冲（14）相对于定时器（24）在脉冲星或其他天体（16）的已知周期被同步平均。 定时器（24）通过将脉冲信号（14）与脉冲形状模板（52）进行比较来测量到达脉冲传感器（22）的脉冲时间，并且处理装置（30）计算测量脉冲时间 到达传感器（22）的计算脉冲时间到达太阳系重心（SSBC）。 脉冲星（16）的位置和脉冲轮廓特征被存储在数字存储器（34）中，并将计算出的时间偏移与脉冲星（16）的已知位置，航天器（12）的导航位置，速度，姿态和时间 ）可以计算出SSBC。

公开(公告)号：US20050192719A1

公开(公告)日：2005-09-01

申请号：US10728869

申请日：2003-12-08

申请人： Suneel Ismail Sheikh ,  Darryll John Pines ,  Kent Wood ,  Paul Shelton Ray ,  Michael Lovellette

发明人： Suneel Ismail Sheikh ,  Darryll John Pines ,  Kent Wood ,  Paul Shelton Ray ,  Michael Lovellette

IPC分类号： B64G1/36 ,  G06F7/00

CPC分类号： B64G1/36

摘要： A system and method for navigation utilizing sources of pulsed celestial radiation are provided. A spacecraft, satellite, or other vehicle (12) has a pulse sensor (22) mounted thereto for detecting signal pulses (14) generated by a plurality of pulsars or other celestial objects (16). The detected signal pulses (14) are synchronously averaged at the known period of the pulsar or other celestial object (16) with respect to a timer (24). Timer (24) measures the pulse time of arrival at the pulse sensor (22) by comparing the pulse signal (14) with a pulse shape template (52), and a processing means (30) calculates the offset time between the measured pulse time of arrival at sensor (22) with a calculated pulse time of arrival at the solar system barycenter (SSBC). The positions and pulse profile characteristics of the pulsars (16) are stored in a digital memory (34) and combining the calculated time offset with the known positions of pulsars (16), the navigational position, velocity, attitude and time of spacecraft (12) with respect to the SSBC can be calculated.

摘要翻译： 提供了利用脉冲天体辐射源的导航系统和方法。 航天器，卫星或其他车辆（12）具有安装在其上的脉冲传感器（22），用于检测由多个脉冲星或其他天体（16）产生的信号脉冲（14）。 所检测的信号脉冲（14）相对于定时器（24）在脉冲星或其他天体（16）的已知周期被同步平均。 定时器（24）通过将脉冲信号（14）与脉冲形状模板（52）进行比较来测量到达脉冲传感器（22）的脉冲时间，并且处理装置（30）计算测量脉冲时间 到达传感器（22）的计算脉冲时间到达太阳系重心（SSBC）。 脉冲星（16）的位置和脉冲轮廓特征被存储在数字存储器（34）中，并将计算出的时间偏移与脉冲星（16）的已知位置，航天器（12）的导航位置，速度，姿态和时间 ）可以计算出SSBC。