正交频分复用(orthogonal frequency division multiplexing,OFDM)信号是雷达通信一体化系统常用的发射波形之一,但是其峰均比较高,影响发射机的工作效率。传统的限幅法虽然可以降低系统OFDM信号的峰均比(peak-to-average power ratio,P...正交频分复用(orthogonal frequency division multiplexing,OFDM)信号是雷达通信一体化系统常用的发射波形之一,但是其峰均比较高,影响发射机的工作效率。传统的限幅法虽然可以降低系统OFDM信号的峰均比(peak-to-average power ratio,PAPR),但会造成误码率(bit error rate,BER)增大和带外频谱泄露的问题。对传统的限幅法进行改进,将高于门限的信号进行抑制,通过迭代滤波消除带外信号弥散造成的频谱效率下降的问题。将改进峰均比抑制方法与传统峰均比抑制方法进行比较,验证了所提方法的低峰均比性能、误码率性能和模糊函数性能。仿真实验表明,所提方法通过合理设置限幅门限和选择迭代滤波次数,可以有效降低OFDM信号的PAPR,并且对雷达探测性能和通信性能影响较小。展开更多
When satellite navigation receivers are equipped with multiple antennas, they can deliver attitude information. In previous researches, carrier phase differencing measurement equations were built in the earth-centered...When satellite navigation receivers are equipped with multiple antennas, they can deliver attitude information. In previous researches, carrier phase differencing measurement equations were built in the earth-centered, earth-fixed (ECEF) co- ordinate, and attitude angles could be obtained through the rotation matrix between the body frame (BF) and the local level frame (LLF). Different from the conventional methods, a hybrid algorithm is presented to resolve attitude parameters utilizing the single differencing (SD) carrier phase equations established in LLF. Assuming that the cycle integer ambiguity is known, the measure- ment equations have attitude analytical resolutions by using simultaneous single difference equations for two in-view satellites. In addition, the algorithm is capable of reducing the search integer space into countable 2D discrete points and the ambiguity function method (AFM) resolves the ambiguity function within the analytical solutions space. In the case of frequency division multiple access (FDMA) for the Russian Global Orbiting Navigation Satellite System (GLONASS), a receiver clock bias estimation is employed to evaluate its carrier phase. An evaluating variable and a weighted factor are introduced to assess the integer ambiguity initialization. By static and dynamic ground experiments, the results show that the proposed approach is effective, with enough accuracy and low computation. It can satisfy attitude determination in cases of GPS alone and combined with GLONASS.展开更多
文摘正交频分复用(orthogonal frequency division multiplexing,OFDM)信号是雷达通信一体化系统常用的发射波形之一,但是其峰均比较高,影响发射机的工作效率。传统的限幅法虽然可以降低系统OFDM信号的峰均比(peak-to-average power ratio,PAPR),但会造成误码率(bit error rate,BER)增大和带外频谱泄露的问题。对传统的限幅法进行改进,将高于门限的信号进行抑制,通过迭代滤波消除带外信号弥散造成的频谱效率下降的问题。将改进峰均比抑制方法与传统峰均比抑制方法进行比较,验证了所提方法的低峰均比性能、误码率性能和模糊函数性能。仿真实验表明,所提方法通过合理设置限幅门限和选择迭代滤波次数,可以有效降低OFDM信号的PAPR,并且对雷达探测性能和通信性能影响较小。
文摘When satellite navigation receivers are equipped with multiple antennas, they can deliver attitude information. In previous researches, carrier phase differencing measurement equations were built in the earth-centered, earth-fixed (ECEF) co- ordinate, and attitude angles could be obtained through the rotation matrix between the body frame (BF) and the local level frame (LLF). Different from the conventional methods, a hybrid algorithm is presented to resolve attitude parameters utilizing the single differencing (SD) carrier phase equations established in LLF. Assuming that the cycle integer ambiguity is known, the measure- ment equations have attitude analytical resolutions by using simultaneous single difference equations for two in-view satellites. In addition, the algorithm is capable of reducing the search integer space into countable 2D discrete points and the ambiguity function method (AFM) resolves the ambiguity function within the analytical solutions space. In the case of frequency division multiple access (FDMA) for the Russian Global Orbiting Navigation Satellite System (GLONASS), a receiver clock bias estimation is employed to evaluate its carrier phase. An evaluating variable and a weighted factor are introduced to assess the integer ambiguity initialization. By static and dynamic ground experiments, the results show that the proposed approach is effective, with enough accuracy and low computation. It can satisfy attitude determination in cases of GPS alone and combined with GLONASS.
