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    • 1. 发明授权
    • Method and apparatus for controlling a transmission power threshold of a satellite communication system
    • 用于控制卫星通信系统的发射功率阈值的方法和装置
    • US06760566B1
    • 2004-07-06
    • US09596811
    • 2000-06-19
    • David A. WrightDennis A. NivensMichael S. MunozReginald JueDominic P. Carrozza
    • David A. WrightDennis A. NivensMichael S. MunozReginald JueDominic P. Carrozza
    • H04B7185
    • H04B7/18543H04B7/18513
    • A method and apparatus for closed-loop power threshold leveling for a satellite communication system. An aspect of the present invention includes a plurality of user earth terminals (UET), a satellite and a network control center (NCC). The NCC polls the UETs to obtain power profile information. When polled, the UELTs form power profile responses and send the responses back to the NCC. The NCC forms a power profile database and statistically analyzes the power profile information to determine an uplink power threshold adjustment. The NCC transmits the uplink power threshold adjustment to the satellite, which adjusts an on-board uplink power level threshold in response to the uplink power threshold adjustment. In systems using mutltiple coding levels, the NCC determines uplink power offset values corresponding to the individual coding levels. The NCC delivers the uplink power offset values to the UETs which update their local power offset values.
    • 一种用于卫星通信系统的闭环功率阈值调平的方法和装置。 本发明的一个方面包括多个用户接地终端(UET),卫星和网络控制中心(NCC)。 NCC轮询UET以获得电源配置文件信息。 当轮询时,UELT形成权力配置文件响应并将响应发送回NCC。 NCC形成功率配置文件数据库并统计分析功率配置文件信息以确定上行链路功率阈值调整。 NCC向卫星发送上行功率阈值调整,其响应于上行链路功率阈值调整来调整板载上行链路功率电平阈值。 在使用多个编码电平的系统中,NCC确定与各个编码电平对应的上行链路功率偏移值。 NCC将上行链路功率偏移值提供给更新其本地功率偏移值的UET。
    • 2. 发明授权
    • Doppler learning phase lock loop for burst demodulator
    • 用于脉冲串解调器的多普勒学习锁相环
    • US06603349B2
    • 2003-08-05
    • US09910162
    • 2001-07-20
    • Dominic P. CarrozzaDavid A. WrightReginald Jue
    • Dominic P. CarrozzaDavid A. WrightReginald Jue
    • H03D300
    • H03D3/241H04L27/2332H04L2027/003H04L2027/0057
    • The present invention is a demodulator and a method of demodulating burst communications. A demodulator (100, 200) includes a phase angle source (18), coupled to a current received burst communication, which provides a phase angle of the current received burst communication; a comparator (20), coupled to the phase angle source and a source of an estimated phase angle, which provides an output signal representing an angular difference between a phase of the current received burst communication and the estimated phase angle; and a phase lock loop (20), coupled to the output signal, which provides the estimated phase angle. The phase lock loop includes a Doppler accumulator (102) which provides a Doppler output which provides compensation in the estimated phase angle for the Doppler effect produced by relative motion between the demodulator and a source of the burst communications.
    • 本发明是一种解调器和解调突发通信的方法。 解调器(100,200)包括相位角源(18),其耦合到当前接收的突发通信,其提供当前接收的突发通信的相位角; 耦合到相位角源的比较器(20)和估计的相位角源,其提供表示当前接收的突发通信的相位与估计的相位角之间的角度差的输出信号; 以及耦合到输出信号的锁相环(20),其提供估计的相位角。 锁相环包括多普勒累加器(102),该多普勒累加器提供多普勒输出,该多普勒输出在由解调器与突发通信源之间的相对运动产生的多普勒效应的估计相位角中提供补偿。
    • 3. 发明授权
    • Onboard initial entry processor for facilitating a satellite communication
    • 板载初始入口处理器,用于促进卫星通信
    • US06697344B1
    • 2004-02-24
    • US09270167
    • 1999-03-16
    • Dominic P. CarrozzaGregory S. CasoVincent C. MorettiReginald JueDavid A. Wright
    • Dominic P. CarrozzaGregory S. CasoVincent C. MorettiReginald JueDavid A. Wright
    • H04B7185
    • H04B7/1858
    • An initial entry processor (40) for use in a processing satellite (12) in a satellite based communications system (10) is provided having a buffer (62), a detection and timing circuit (64) and an identity circuit (66). The buffer (62) stores an initial entry burst (54) transmitted from at least one terrestrial terminal (14) to the processing satellite (12). The detection and timing circuit (64) detects the initial entry burst (54) and determines a time of arrival of the initial entry burst (54) relative to an initial entry burst slot (52). The identity circuit (66) determines an identity of the terrestrial terminal (14) that transmitted the initial entry burst (54) such that the time of arrival is used by the identified terrestrial terminal (14) during subsequent communications with the processing satellite (12).
    • 提供了一种用于基于卫星的通信系统(10)中的处理卫星(12)中的初始入口处理器(40),其具有缓冲器(62),检测和定时电路(64)以及标识电路(66)。 缓冲器(62)存储从至少一个地面终端(14)发送到处理卫星(12)的初始入口突发(54)。 检测和定时电路(64)检测初始入口突发(54)并且确定初始入口突发(54)相对于初始入口突发时隙(52)的到达时间。 身份电路(66)确定发射初始入口突发(54)的地面终端(14)的身份,使得在与处理卫星(12)的后续通信期间由所识别的地面终端(14)使用到达时间 )。
    • 10. 发明授权
    • Synchronization method for a processing communication satellite
    • 处理通信卫星的同步方法
    • US06845085B1
    • 2005-01-18
    • US09408965
    • 1999-09-29
    • David A. WrightStuart T. LinskyGregory S. CasoReginald Jue
    • David A. WrightStuart T. LinskyGregory S. CasoReginald Jue
    • H04L27/20H04B7/185H04B7/212H04J3/00H04L7/00H04L27/36H04J3/06
    • H04B7/18513
    • The present invention provides a highly accurate synchronization method for a satellite communication system (100). The system maintains a downlink symbol counter at an earth terminal and determines a downlink symbol count representative of the time of arrival of a burst transmitted from the earth terminal to a satellite (106, 206). The earth terminal adjusts the downlink symbol counter to correspond to the downlink symbol count (136, 220) upon arrival of a predetermined reference point in a downlink frame. A timing error may initially be determined by launching an entry order wire from the earth terminal to the satellite (116). The timing error may be transmitted to the earth terminal using a correction code which indicates the transmission is early, late, absent, or no change is required (134, 218). The terminal may make additional periodic timing adjustments based on the length of the propagation path between the earth terminal and the satellite (108, 208). The earth terminal may then precisely time the transmission of bursts from the earth terminal to the satellite (130, 214). The length of the propagation path and the timing error may be stored in the earth terminal so that the earth terminal may reenter the system without undertaking multiple commissioning processes.
    • 本发明提供了一种用于卫星通信系统(100)的高精度同步方法。 该系统在接地终端维护下行链路符号计数器,并确定表示从地球终端向卫星(106,206)发送的脉冲串的到达时间的下行链路符号计数。 接地终端在下行链路帧中预定参考点到达时,调整下行链路符号计数器以对应于下行链路符号计数(136,220)。 最初可以通过从地球终端向卫星(116)发射入口命令线来确定定时错误。 定时误差可以使用指示传输是早,晚,不存在或不需要改变的校正码(134,218)来发送到接地终端。 终端可以基于接地终端和卫星(108,208)之间的传播路径的长度来进行附加的周期性定时调整。 然后,接地终端可以精确地将从地球终端到突发的传输时间延时到卫星(130,214)。 传播路径的长度和定时误差可以存储在接地端子中,使得接地端子可以重新进入系统而不进行多次调试过程。