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    • 1. 发明授权
    • Satellite communication system
    • 卫星通信系统
    • US07751779B2
    • 2010-07-06
    • US11642713
    • 2006-12-21
    • Hau H. HoEthan A. SteinMichael FashanoPeter J. HadingerGary Lehto
    • Hau H. HoEthan A. SteinMichael FashanoPeter J. HadingerGary Lehto
    • H04Q7/20
    • H04B7/18515
    • A payload (108) to be mounted onto a satellite (102) can include a first steerable antenna (302) providing a downlink to and an uplink from a first user terminal; a second steerable antenna (304) providing a downlink to and an uplink from a second user terminal; a switching network (306) coupling the first steerable antenna to the second steerable antenna; and a payload control unit (120) controlling the switching network to select one of the downlink to the first user terminal provided by the first steerable antenna and the downlink to the second user terminal provided by the second steerable antenna, and one of the uplink from the first user terminal provided by the first steerable antenna and the uplink from the second user terminal provided by the second steerable antenna.
    • 要安装到卫星(102)上的有效载荷(108)可以包括向第一用户终端提供下行链路和上行链路的第一可操纵天线(302) 向第二用户终端提供下行链路和上行链路的第二可控天线(304) 交换网络(306),将所述第一可转向天线耦合到所述第二可转向天线; 以及有效负载控制单元(120),其控制所述交换网络,以选择由所述第一可操纵天线提供的所述第一用户终端的下行链路和由所述第二可控天线提供的所述第二用户终端的下行链路,以及所述上行链路中的一个 由第一可操纵天线提供的第一用户终端和由第二可控天线提供的来自第二用户终端的上行链路。
    • 2. 发明申请
    • Satellite communication system
    • 卫星通信系统
    • US20080153414A1
    • 2008-06-26
    • US11642713
    • 2006-12-21
    • Hau H. HoEthan A. SteinMichael FashanoPeter J. HadingerGary Lehto
    • Hau H. HoEthan A. SteinMichael FashanoPeter J. HadingerGary Lehto
    • H04B7/185
    • H04B7/18515
    • A payload (108) to be mounted onto a satellite (102) can include a first steerable antenna (302) providing a downlink to and an uplink from a first user terminal; a second steerable antenna (304) providing a downlink to and an uplink from a second user terminal; a switching network (306) coupling the first steerable antenna to the second steerable antenna; and a payload control unit (120) controlling the switching network to select one of the downlink to the first user terminal provided by the first steerable antenna and the downlink to the second user terminal provided by the second steerable antenna, and one of the uplink from the first user terminal provided by the first steerable antenna and the uplink from the second user terminal provided by the second steerable antenna.
    • 要安装到卫星(102)上的有效载荷(108)可以包括向第一用户终端提供下行链路和上行链路的第一可操纵天线(302) 向第二用户终端提供下行链路和上行链路的第二可控天线(304) 交换网络(306),将所述第一可转向天线耦合到所述第二可转向天线; 以及有效负载控制单元(120),其控制所述交换网络,以选择由所述第一可操纵天线提供的所述第一用户终端的下行链路和由所述第二可控天线提供的所述第二用户终端的下行链路,以及所述上行链路中的一个 由第一可操纵天线提供的第一用户终端和由第二可控天线提供的来自第二用户终端的上行链路。
    • 6. 发明授权
    • Code modulation using narrow spectral notching
    • 使用窄谱切割的码调制
    • US06631165B1
    • 2003-10-07
    • US09388175
    • 1999-09-01
    • Russell H. LambertPeter J. HadingerDenes L. ZsolnayBruce W. EvansShi-Ping HsuGerard Roccanova
    • Russell H. LambertPeter J. HadingerDenes L. ZsolnayBruce W. EvansShi-Ping HsuGerard Roccanova
    • H04L2700
    • H04H20/14H04H20/31H04L27/00
    • A method (100) and apparatus (400) for encoding and decoding data in a signal using notch depth modulation. The method (100) of data to be encoded in the signal. The method then notch filters (125) the signal according to the frequency notch representation of the data. The apparatus (400) for encoding data comprises an digitizer (405) to digitize the signal. A code former (420) provides the data to be encoded in the signal. A notch filter (430) notch filters the signal according to the data. Decoding the data converts the signal into a frequency domain representation (520) and determines the notch spectral content (525) of the signal at selected notch frequencies. The method (500) establishes notch thresholds (534) at each of the selected notch frequencies, then decodes the data (540) from the signal by comparing the notch spectral content to the notch thresholds.
    • 一种用于使用陷波深度调制对信号中的数据进行编码和解码的方法(100)和装置(400)。 在信号中要编码的数据的方法(100)。 该方法然后根据数据的频率陷波表示来陷波滤波器(125)信号。 用于编码数据的装置(400)包括用于数字化信号的数字化仪(405)。 代码表(420)提供要在信号中编码的数据。 陷波滤波器(430)根据数据对信号进行陷波滤波。 对数据进行解码将信号转换为频域表示(520),并确定所选陷波频率处的信号的陷波频谱含量(525)。 方法(500)在每个选择的陷波频率处建立陷波阈值(534),然后通过将陷波频谱内容与陷波阈值进行比较来解码来自信号的数据(540)。
    • 7. 发明授权
    • Satellite multimedia delivery to vehicles
    • 卫星多媒体传送到车辆
    • US06512921B1
    • 2003-01-28
    • US09562504
    • 2000-05-01
    • Peter J. Hadinger
    • Peter J. Hadinger
    • H04Q720
    • H04B7/1858
    • A GSO satellite constellation (10) and an NGSO constellation (20) may be used to send various types of communication signals and multimedia signals to an aircraft (30). The video signals are demodulated by a demodulator (46) and routed by a router (64) to TV monitors (72 and 74), as well as short-term video storage (78). Data can be received and transmitted by a low gain, narrowband transmitter/receiver (100) in order to provide voice, computer and control communications at all times during the flight of aircraft (30).
    • 可以使用GSO卫星星座(10)和NGSO星座(20)向飞机(30)发送各种类型的通信信号和多媒体信号。 视频信号由解调器(46)解调并由路由器(64)路由到TV监视器(72和74)以及短期视频存储(78)。 可以通过低增益窄带发射机/接收机(100)接收和传输数据,以便在飞机(30)飞行期间的任何时候提供语音,计算机和控制通信。