首页> 外国专利> METHOD FOR DETERMINATION OF GEOGRAPHIC POSITION OF OBSERVED AREA OF OBSERVATION EQUIPMENT BEING MOVED RELATIVE TO SPACECRAFT, SYSTEM FOR ITS IMPLEMENTATION AND DEVICE FOR ARRANGING EMITTERS ON OBSERVATION EQUIPMENT

METHOD FOR DETERMINATION OF GEOGRAPHIC POSITION OF OBSERVED AREA OF OBSERVATION EQUIPMENT BEING MOVED RELATIVE TO SPACECRAFT, SYSTEM FOR ITS IMPLEMENTATION AND DEVICE FOR ARRANGING EMITTERS ON OBSERVATION EQUIPMENT

机译:确定相对于航天飞机移动的观测设备的观测区域的地理位置的方法,其实现系统和在观测设备上布置辐射器的装置

摘要

FIELD: transport.;SUBSTANCE: invention relates to space engineering. Method for determination of geographic position of observed area of observation equipment being moved relative to SC includes navigational measurements of SC movement, determination of centre of mass position and SC orientation, determination of observation equipment spatial position. Additionally, control commands are generated for emitting pulse ultrasonic signals by at least three emitters located in spaced points on observation equipment freely moved relative to SC, emitted pulse ultrasonic signals are received by at least three ultrasonic receivers located in spaced points on SC. Ultrasonic signal delay time is measured on the basis of emitted and received ultrasonic signals. Synchronisation of pulse ultrasonic signal emission and receive times is performed via radio channel. Temperature measurement is performed at locations of ultrasonic emitters and at locations of ultrasonic receivers. On the basis of ultrasonic signal receive delay times and measured temperatures the distances form ultrasonic emitters to ultrasonic receivers are determined. Geographic position of observation area is determined on the basis of SC centre of mass position relative to planet, SC orientation relative to planet and spatial position of observation equipment relative to SC calculated from distances from ultrasonic emitters to ultrasonic receivers. System for determination of geographic position of observed area of observation equipment being moved relative to SC includes SC centre of mass position determination unit, SC orientation determination unit, observed area geographic position determination unit. Additionally, following devices are introduced: at least three ultrasonic emitters and at least one temperature sensor installed on observation equipment, at least three ultrasonic receivers and at least one temperature sensor installed on SC, emitter control command generation unit, controllers, radio transceivers, signal amplifier, automatic gain control unit, multichannel analogue-to-digital converter, signal delay time measurement unit, synchroniser, unit for determination of observation equipment spatial position relative to SC. Device for emitters arrangement on observation equipment contains detachable connection one of detachable parts of which is rigidly connected with observation equipment. Additionally, at least three pillars are introduced on each one of which ultrasonic emitters are installed. The pillars are rigidly connected with the other detachable part of detachable connection. Emission axes of ultrasonic emitters are parallel to observation equipment sensing axis. Distances from ultrasonic emitters to observation equipment sensing axis are selected by proposed formula depending on dimensions of observation equipment lens and SC window through which observations are performed and on minimum distance from observation equipment to the window.;EFFECT: highly precise determination of geographic position of area being observed through observation equipment freely moved in zero gravity conditions relative to SC and having no mechanical connection with SC, while providing possibility to use various exchangeable observation devices.;3 cl, 3 dwg
机译:技术领域本发明涉及空间工程。用于确定相对于SC移动的观察设备的观察区域的地理位置的方法包括:对SC运动的导航测量,确定质心位置和SC方向,确定观察设备的空间位置。另外,产生控制命令以通过位于相对于SC自由移动的观察设备上的间隔点中的至少三个发射器发射脉冲超声信号,通过位于SC上的间隔点中的至少三个超声接收器接收发射的脉冲超声信号。超声波信号延迟时间是根据发射和接收的超声波信号测量的。脉冲超声波信号发射和接收时间的同步是通过无线电信道执行的。在超声发射器的位置和超声接收器的位置执行温度测量。基于超声波信号接收延迟时间和所测量的温度,确定从超声波发射器到超声波接收器的距离。根据从超声波发射器到超声波接收器的距离计算得出的相对于行星的质量中心位置,相对于行星的SC方向以及相对于SC的观测设备的空间位置,确定观测区域的地理位置。用于确定相对于SC移动的观察设备的观察区域的地理位置的系统包括SC质心位置确定单元,SC取向确定单元,观察区域地理位置确定单元。此外,还引入了以下设备:至少三个超声波发射器和至少一个安装在观测设备上的温度传感器,至少三个超声波接收器和至少一个安装在SC上的温度传感器,发射器控制命令生成单元,控制器,无线电收发器,信号放大器,自动增益控制单元,多通道模数转换器,信号延迟时间测量单元,同步器,用于确定观测设备相对于SC的空间位置的单元。用于在观察设备上布置发射器的设备包含可拆卸连接,该设备的可拆卸部分之一与观察设备刚性连接。另外,在每个超声波发射器上安装至少三个支柱。支柱与可拆卸连接的另一可拆卸部分刚性连接。超声波发射器的发射轴平行于观测设备感测轴。超声波发射器到观测设备感应轴的距离是根据建议的公式来选择的,具体取决于观测设备镜头和SC窗口的尺寸,并通过该窗口进行观测,以及从观测设备到窗口的最小距离。通过在零重力条件下相对于SC自由移动且与SC没有机械连接的观察设备观察到的区域,同时提供了使用各种可互换观察装置的可能性; 3 cl,3 dwg

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