摘要:
A space navigation receiver (NR) comprises i) a radiofrequency processing module (PM1) tasked both with converting radio navigation signals transmitted by a satellite navigation system into digital navigation signals, and with converting auxiliary radio signals representative of navigation information about said system into auxiliary digital signals, ii) a digital processing module (PM2) tasked with periodically acquiring the digital navigation signals by sub-sampling the received radio signal, then processing the acquired signal samples (resulting from this sub-sampling) in order to produce raw measurements from these samples, from auxiliary digital signals, and from location points, and iii) a location module (LM) tasked with determining location points based on raw measurements, demodulated navigation data initially contained within the digital navigation signals in a modulated form, and orbital force models.
摘要:
A space navigation receiver (NR) comprises i) a radiofrequency processing module (PM1) tasked both with converting radio navigation signals transmitted by a satellite navigation system into digital navigation signals, and with converting auxiliary radio signals representative of navigation information about said system into auxiliary digital signals, ii) a digital processing module (PM2) tasked with periodically acquiring the digital navigation signals by sub-sampling the received radio signal, then processing the acquired signal samples (resulting from this sub-sampling) in order to produce raw measurements from these samples, from auxiliary digital signals, and from location points, and iii) a location module (LM) tasked with determining location points based on raw measurements, demodulated navigation data initially contained within the digital navigation signals in a modulated form, and orbital force models.
摘要:
The method makes it possible digitally to evaluate the phase of any carrier that has been subjected to rPSK modulation subsequent to clock recovery, sampling, and digitizing the in-phase and quadrature components of the samples, by processing that is performed in polar coordinates and that comprises reducing the range over which the phase of each sample is defined to a range of +.pi./r to -.pi./r and then seeking the center of gravity over 2.sup.N successive samples (N being an integer) by performing successive averaging calculations, each time on two values, in application of an N-stage tree structure. Each average of two values is associated with an index indicative of the degree of reliability of the average, and those averages which are associated with a small reliability index are ignored while calculating subsequent averages in the tree structure.
摘要翻译:该方法可以通过在极坐标中进行的处理来对采样的同相和正交分量进行时钟恢复,采样和数字化之后经过rPSK调制的任何载波的相位进行评估, 包括将每个样本的相位定义的范围减小到+ pi / r至-pi / r的范围,然后通过执行连续的平均计算来寻求超过2N个连续样本(N为整数)的重心 时间在两个值,应用N阶段树结构。 两个值的平均值与指示平均值的可靠度的指标相关联,并且在计算树结构中的后续平均值时忽略与小可靠性指数相关联的那些平均值。
摘要:
In order to detect the error on the frequency of an M-PSK phase-modulated carrier, the phase .psi.(n) of the samples is restored to the interval �-.pi., +.pi.�; .phi.(n)=mod(.psi.(n), 2.pi./M) is calculated; d(n)=mod(.phi.(n)-.phi.(n-1), 2.pi./M) is calculated; p'(n)=mod(d(n)+p(n-1), 2.pi./M) is calculated, where p(n)=mod(p*(n), 2.pi./M), where p*(n) is obtained by subtracting the current output from p'(n); d'(n)=p'(n)-p(n-1) is calculated; a parameter "tri" is defined by tri=1 if .vertline.d'(n).vertline.
摘要翻译:为了检测M-PSK相位调制载波的频率误差,采样的相位psi(n)恢复到间隔[ - pi,+ pi [ 计算phi(n)= mod(psi(n),2π/ M) d(n)= mod(phi(n)-phi(n-1),2π/ M) p(n)= mod(d(n)+ p(n-1),2 pi / M),其中p(n)= mod 通过从p'(n)减去电流输出获得*(n); d'(n)= p'(n)-p(n-1); 如果| d'(n)| / = S,则三角形为三角形,其中S为阈值; (n)=α.p'(n).tri被计算,构成电流输出的det-tri(n)代表载波频率上的误差。
摘要:
A method and a system for locating ground equipment transmitting signals to a geostationary satellite, the method and the system being based on identifying the arrival directions of such signals within the coverage zone of the satellite. In the method, the arrival directions of the signals are identified by using a beam-forming active-module array antenna system on board the satellite, the system being controlled to define simultaneous beams in the radiation pattern of the antenna, the beams being superposed on one another with small offsets, the superposed beams corresponding to a limited analysis zone being illuminated within the coverage zone of the satellite, the system further being associated with a digital processing program which identifies the arrival directions of the signals which are received in the analysis zone.