公开(公告)号：EP0513349A1

公开(公告)日：1992-11-19

申请号：EP90908151.5

申请日：1990-01-30

申请人： NAUCHNO-ISSLEDOVATELSKY INSTITUT KOSMICHESKOGO PRIBOROSTROENIA

发明人： ALYABIN, German Mikhailovich ,  VOLKOV, Nikolai Mikhailovich ,  GLAZOV, Stanislav Sergeevich ,  IVANOV, Nikolai Emelyanovich ,  KOVALENKO, Valery Filippovich ,  LJUBIMOV, Mikhail Alexandrovich ,  SALISCHEV, Vadim Alexandrovich ,  SERGEEV, Boris Georgievich ,  TJUBALIN, Valery Vasilievich

IPC分类号： G01S5/14

CPC分类号： G01S19/21 ,  G01S19/02 ,  H02H3/066 ,  H02H3/0935 ,  H02H9/001 ,  H02M5/293

摘要： A method for radio-navigational determinations using artificial Earth-satellites for generation on satellites (1) of a radio-navigational signal by means of modulation of the carrier frequency (f c ) by a combination of signals comprising a pseudorandom sequence, navigational data and a synchrocode, and the object/users (2) receiving and processing the radio-navigational signals to determine their co-ordinates, speed and correction to the time scale of the object. According to the invention, an individual carrier frequency (f cj , f ck ) is used for each satellite or for each pair of satellites (1) mutually opposite in the orbit plane; a common pseudorandom M-sequence with a lower number of elements is used for all the satellites (1) and a bi-binary coding of the navigation data symbols is used as well as a synchrocode with a decreased repetition period and with an increased number of symbols. According to the invention, a satellite radio-navigational system on each satellite (1) in a subsystem for generating and transmitting the radio-navigational signal, and on an object/user for (2) in a subsystem for receiving and processing the radio-navigational signal, implements fully the claimed method, thus increasing the probability of high precision navigational determinations at any moment of time due to practically complete exclusion of intrasystem interference, and essentially decreasing the time needed for the navigational determination.

摘要翻译： 一种使用人造地球卫星在无线电导航信号的卫星（1）上进行无线电导航确定的方法，其通过包括伪随机序列，导航数据和导频数据的信号的组合来调制载波频率（fc） 同步码，以及对象/用户（2）接收和处理无线电导航信号以确定其坐标，速度和对对象时间尺度的校正。 根据本发明，对于每个卫星或在轨道平面中彼此相对的每对卫星（1）使用单个载波频率（fcj，fck）; 对于所有卫星（1）使用具有较少数量元素的通用伪随机M序列，并且使用导航数据符号的二进制编码以及具有减少的重复周期和增加的数量的同步码 符号。 根据本发明，在用于生成和发送无线电导航信号的子系统中的每个卫星（1）上的卫星无线电导航系统，以及用于（2）在子系统中的用于接收和处理无线电导航信号的子系统中的卫星无线电导航系统， 导航信号完全实现了所要求的方法，因此由于实际上完全排除了系统内干扰，并且基本上减少了导航确定所需的时间，从而增加了任何时刻的高精度导航确定的可能性。

公开(公告)号：EP0513349B1

公开(公告)日：1996-11-20

申请号：EP90908151.5

申请日：1990-01-30

申请人： NAUCHNO-ISSLEDOVATELSKY INSTITUT KOSMICHESKOGO PRIBOROSTROENIA

发明人： ALYABIN, German Mikhailovich ,  VOLKOV, Nikolai Mikhailovich ,  GLAZOV, Stanislav Sergeevich ,  IVANOV, Nikolai Emelyanovich ,  KOVALENKO, Valery Filippovich ,  LJUBIMOV, Mikhail Alexandrovich ,  SALISCHEV, Vadim Alexandrovich ,  SERGEEV, Boris Georgievich ,  TJUBALIN, Valery Vasilievich

IPC分类号： G01S5/14

CPC分类号： G01S19/21 ,  G01S19/02 ,  H02H3/066 ,  H02H3/0935 ,  H02H9/001 ,  H02M5/293

摘要： A method for radio-navigational determinations using artificial Earth-satellites providing for generation on satellites (1) of a radio-navigational signal by means of modulation of the carrier frequency (fc) by a combination of signals comprising a pseudorandom sequence, navigational data and a synchrocode, and the object/users (2) receiving and processing the radio-navigational signals to determine their co-ordinates, speed and correction to the time scale of the object. According to the invention, an individual carrier frequency (fcj, fck) is used for each satellite or for each pair of satellites (1) mutually opposite in the orbit plane; a common pseudorandom M-sequence with a lower number of elements is used for all the satellites (1) and a bi-binary coding of the navigation data symbols is used as well as a synchrocode with a decreased repetition period and with an increased number of symbols. According to the invention, a satellite radio-navigational system on each satellite (1) in a subsystem for generating and transmitting the radio-navigational signal, and on an object/user (2) in a subsystem for receiving and processing the radio-navigational signal, implements fully the claimed method, thus increasing the probability of high precision navigational determinations at any moment of time due to practically complete exclusion of intrasystem interference, and essentially decreasing the time needed for the navigational determination.