The tracking, telemetry and command （TT＆C） mission is extremely reliable for its characters of small time horizon and high redundancy. The combined forcing and failure biasing （CFFB） method that is usually used f...The tracking, telemetry and command （TT＆C） mission is extremely reliable for its characters of small time horizon and high redundancy. The combined forcing and failure biasing （CFFB） method that is usually used for simulating the unreliability of the highly dependable mission system seems not so efficient for the TT＆C mission. The concept about the importance of failure transition is proposed based on the logical relationship between TT＆C mission and its involved resources. Then, the importance is used for readjusting the transition rate of the failure transition when using the forcing and failure biasing during the simulation. Examples show that the improved CFFB method can evidently increase the occurrence of the TT＆C mission failure event and decrease the sample variance. More redundancy of the TT＆C mission leads to the improved CFFB method more efficient.展开更多
An interference mitigation for acquisition method,based on both energy center and spectrum symmetry detection,has been proposed as a possible solution to the problem of signal acquisition susceptibility to continuous-...An interference mitigation for acquisition method,based on both energy center and spectrum symmetry detection,has been proposed as a possible solution to the problem of signal acquisition susceptibility to continuous-wave interference(CWI)in unified carrier telemetry,tracking,and command(TT&C)systems.With subcarrier modulation index as a priori condition,the existence of CWI is determined by comparing the energy center with the symmetric center.In the presence of interference,the interference frequency point is assumed and culled;sequentially,the spectral symmetry is used to verify whether the signal acquisition is realized.Theoretical analysis,simulations,and experimental results demonstrate that the method can realize the acquisition of the main carrier target signal with an interference-to-signal ratio of 31 dB,which represents an improvement over the existing continuous-wave interference mitigation for acquisition methods.展开更多
随着我国航天测控(Tracking Telemetry and Command, TT&C)领域的不断发展,面向全空域相控阵TT&C的工程应用越来越多,传统TT&C系统中的校相及跟踪方法无法适应新的工程应用。针对目前全空域相控阵TT&C系统中校相及目标...随着我国航天测控(Tracking Telemetry and Command, TT&C)领域的不断发展,面向全空域相控阵TT&C的工程应用越来越多,传统TT&C系统中的校相及跟踪方法无法适应新的工程应用。针对目前全空域相控阵TT&C系统中校相及目标跟踪方法与传统TT&C系统不通用的问题,结合工程实践应用,介绍了全空域相控阵TT&C系统中的校相及目标跟踪方法。实践表明,所提方法具有良好的目标跟踪能力,可满足工程需要。展开更多
航天测控通信网自建成以来,整体运行较为稳定,但在网络安全方面也暴露出了一些问题,为研究和解决目前航天测控通信网中存在的网络安全问题,在分析TCP/IP(Transmission Control Protocol/Intcrnct Protocol,传输控制协议/互联网协议)分...航天测控通信网自建成以来,整体运行较为稳定,但在网络安全方面也暴露出了一些问题,为研究和解决目前航天测控通信网中存在的网络安全问题,在分析TCP/IP(Transmission Control Protocol/Intcrnct Protocol,传输控制协议/互联网协议)分层协议基本原理的基础上,研究了IP网数据链路层、网络层和传输层的协议漏洞及常见攻击方法,详细介绍了当前航天测控通信网的网络安全部署情况,根据网络现状分别对航天测控通信网上数据链路层、网络层和传输层存在的安全问题进行了纵向分析,针对分析出的各类安全问题,进一步给出了有效的防御措施和防护方法。最后,探讨提出了一套航天测控通信网配置维护管理系统的设计方案,通过建立设备配置信息库、检查信息记录库及网络故障库等,实现了对航天测控通信网安全稳定运行的有效管理。展开更多
针对连线干涉测量系统(CEI)在无模型时延或模型时延不准确条件下相位模糊度解算困难的问题,提出了利用伪码测距信号辅助的载波相位模糊解算方法。在测站距离约束下,根据两站所接收伪码信号的相对位置关系计算得到一个时延差作为解载波...针对连线干涉测量系统(CEI)在无模型时延或模型时延不准确条件下相位模糊度解算困难的问题,提出了利用伪码测距信号辅助的载波相位模糊解算方法。在测站距离约束下,根据两站所接收伪码信号的相对位置关系计算得到一个时延差作为解载波相位模糊的时延预报值。为了提高解模糊能力,引入了伪码捕获和跟踪的基本方法。仿真分析了不同信噪比下所能达到的最大精度,结果表明在信噪比高于0 d B时,可直接解算S频段的载波相位模糊;在信噪比较低时,可解算宽带群时延的相位模糊。在0 d B和-30 d B条件下重复试验1 000次,正确率分别达到99.88%和99.91%,证明了算法的有效性。展开更多
The envelope of a hypersonic vehicle is affected by severe fluctuating pressure, which causes the airborne antenna to vibrate slightly. This vibration mixes with the transmitted signals and thus introduces additional ...The envelope of a hypersonic vehicle is affected by severe fluctuating pressure, which causes the airborne antenna to vibrate slightly. This vibration mixes with the transmitted signals and thus introduces additional multiplicative phase noise. Antenna vibration and signal coupling effects as well as their influence on the lock threshold of the hypersonic vehicle carrier tracking system of the Ka band are investigated in this study. A vibration model is initially established to obtain phase noise in consideration of the inherent relationship between vibration displacement and electromagnetic wavelength. An analytical model of the Phase-Locked Loop（PLL）, which is widely used in carrier tracking systems, is established. The coupling effects on carrier tracking performance are investigated and quantitatively analyzed by imposing the multiplicative phase noise on the PLL model. Simulation results show that the phase noise presents a Gaussian distribution and is similar to vibration displacement variation. A large standard deviation in vibration displacement exerts a significant effect on the lock threshold. A critical standard deviation is observed in the PLL of Binary Phase Shift Keying（BPSK） and Quadrature Phase Shift Keying（QPSK） signals. The effect on QPSK signals is more severe than that on BPSK signals. The maximum tolerable standard deviations normalized by the wavelength of the carrier are 0.04 and 0.02 for BPSK and QPSK signals,respectively. With these critical standard deviations, lock thresholds are increased from à12 andà4 d B to 3 and à2 d B, respectively.展开更多
基金supported by the National Natural Science Foundation of China (71071159)
文摘The tracking, telemetry and command （TT＆C） mission is extremely reliable for its characters of small time horizon and high redundancy. The combined forcing and failure biasing （CFFB） method that is usually used for simulating the unreliability of the highly dependable mission system seems not so efficient for the TT＆C mission. The concept about the importance of failure transition is proposed based on the logical relationship between TT＆C mission and its involved resources. Then, the importance is used for readjusting the transition rate of the failure transition when using the forcing and failure biasing during the simulation. Examples show that the improved CFFB method can evidently increase the occurrence of the TT＆C mission failure event and decrease the sample variance. More redundancy of the TT＆C mission leads to the improved CFFB method more efficient.
基金Supported by the National Natural Science Foundation of China(61401026)
文摘An interference mitigation for acquisition method,based on both energy center and spectrum symmetry detection,has been proposed as a possible solution to the problem of signal acquisition susceptibility to continuous-wave interference(CWI)in unified carrier telemetry,tracking,and command(TT&C)systems.With subcarrier modulation index as a priori condition,the existence of CWI is determined by comparing the energy center with the symmetric center.In the presence of interference,the interference frequency point is assumed and culled;sequentially,the spectral symmetry is used to verify whether the signal acquisition is realized.Theoretical analysis,simulations,and experimental results demonstrate that the method can realize the acquisition of the main carrier target signal with an interference-to-signal ratio of 31 dB,which represents an improvement over the existing continuous-wave interference mitigation for acquisition methods.
文摘随着我国航天测控(Tracking Telemetry and Command, TT&C)领域的不断发展,面向全空域相控阵TT&C的工程应用越来越多,传统TT&C系统中的校相及跟踪方法无法适应新的工程应用。针对目前全空域相控阵TT&C系统中校相及目标跟踪方法与传统TT&C系统不通用的问题,结合工程实践应用,介绍了全空域相控阵TT&C系统中的校相及目标跟踪方法。实践表明,所提方法具有良好的目标跟踪能力,可满足工程需要。
文摘航天测控通信网自建成以来,整体运行较为稳定,但在网络安全方面也暴露出了一些问题,为研究和解决目前航天测控通信网中存在的网络安全问题,在分析TCP/IP(Transmission Control Protocol/Intcrnct Protocol,传输控制协议/互联网协议)分层协议基本原理的基础上,研究了IP网数据链路层、网络层和传输层的协议漏洞及常见攻击方法,详细介绍了当前航天测控通信网的网络安全部署情况,根据网络现状分别对航天测控通信网上数据链路层、网络层和传输层存在的安全问题进行了纵向分析,针对分析出的各类安全问题,进一步给出了有效的防御措施和防护方法。最后,探讨提出了一套航天测控通信网配置维护管理系统的设计方案,通过建立设备配置信息库、检查信息记录库及网络故障库等,实现了对航天测控通信网安全稳定运行的有效管理。
文摘针对连线干涉测量系统(CEI)在无模型时延或模型时延不准确条件下相位模糊度解算困难的问题,提出了利用伪码测距信号辅助的载波相位模糊解算方法。在测站距离约束下,根据两站所接收伪码信号的相对位置关系计算得到一个时延差作为解载波相位模糊的时延预报值。为了提高解模糊能力,引入了伪码捕获和跟踪的基本方法。仿真分析了不同信噪比下所能达到的最大精度,结果表明在信噪比高于0 d B时,可直接解算S频段的载波相位模糊;在信噪比较低时,可解算宽带群时延的相位模糊。在0 d B和-30 d B条件下重复试验1 000次,正确率分别达到99.88%和99.91%,证明了算法的有效性。
基金co-supported by the National Basic Research Program of China (No. 2014CB340205)the Natural Science Foundation of Shaanxi Provincial Department of Education (No. 2016JM6016)the National Natural Science Foundation of China (No. 61473228)
文摘The envelope of a hypersonic vehicle is affected by severe fluctuating pressure, which causes the airborne antenna to vibrate slightly. This vibration mixes with the transmitted signals and thus introduces additional multiplicative phase noise. Antenna vibration and signal coupling effects as well as their influence on the lock threshold of the hypersonic vehicle carrier tracking system of the Ka band are investigated in this study. A vibration model is initially established to obtain phase noise in consideration of the inherent relationship between vibration displacement and electromagnetic wavelength. An analytical model of the Phase-Locked Loop（PLL）, which is widely used in carrier tracking systems, is established. The coupling effects on carrier tracking performance are investigated and quantitatively analyzed by imposing the multiplicative phase noise on the PLL model. Simulation results show that the phase noise presents a Gaussian distribution and is similar to vibration displacement variation. A large standard deviation in vibration displacement exerts a significant effect on the lock threshold. A critical standard deviation is observed in the PLL of Binary Phase Shift Keying（BPSK） and Quadrature Phase Shift Keying（QPSK） signals. The effect on QPSK signals is more severe than that on BPSK signals. The maximum tolerable standard deviations normalized by the wavelength of the carrier are 0.04 and 0.02 for BPSK and QPSK signals,respectively. With these critical standard deviations, lock thresholds are increased from à12 andà4 d B to 3 and à2 d B, respectively.
