WO2014100989A1 - 一种天线*** - Google Patents
一种天线*** Download PDFInfo
- Publication number
- WO2014100989A1 WO2014100989A1 PCT/CN2012/087486 CN2012087486W WO2014100989A1 WO 2014100989 A1 WO2014100989 A1 WO 2014100989A1 CN 2012087486 W CN2012087486 W CN 2012087486W WO 2014100989 A1 WO2014100989 A1 WO 2014100989A1
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- WIPO (PCT)
- Prior art keywords
- antenna
- reflector
- transmitting
- receiving
- receiving antenna
- Prior art date
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- 230000005540 biological transmission Effects 0.000 claims description 12
- 239000004020 conductor Substances 0.000 claims description 6
- 238000004891 communication Methods 0.000 abstract description 7
- 230000002452 interceptive effect Effects 0.000 abstract 2
- 238000010586 diagram Methods 0.000 description 7
- 239000010410 layer Substances 0.000 description 5
- 238000001228 spectrum Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 3
- 238000002955 isolation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 239000003989 dielectric material Substances 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/52—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure
- H01Q1/521—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure reducing the coupling between adjacent antennas
- H01Q1/525—Means for reducing coupling between antennas; Means for reducing coupling between an antenna and another structure reducing the coupling between adjacent antennas between emitting and receiving antennas
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/42—Housings not intimately mechanically associated with radiating elements, e.g. radome
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B15/00—Suppression or limitation of noise or interference
Definitions
- the present invention relates to the field of communications, and in particular, to an antenna system. Background technique
- Microwave communication equipment usually uses different frequencies to simultaneously transmit and receive signals. This spectrum utilization method causes waste of spectrum resources.
- the resulting full-duplex communication technology that is, data transmission on the same spectrum, and spectrum utilization of data reception, can greatly improve the utilization efficiency of the spectrum.
- a key issue in full-duplex communication is that the transmitting antenna of the device will generate co-channel interference to the receiving antenna of the local end due to the same frequency of transmission and reception, and the same-frequency interference cannot be suppressed by the filter. Therefore, improving the isolation between the transceiver antennas of the device is a key issue to be solved for full-duplex communication.
- the solution uses two transmit antennas TX1 and TX2 and one receive antenna RX.
- the difference between the distance between the two transmitting antennas and the receiving antenna is '2, where is the wavelength of the carrier.
- the signals transmitted by the transmitting antennas TX1 and TX2 are received by the receiving antenna RX, thereby generating co-channel interference.
- the transmitted signal is divided into two identical signals by the power splitter and fed into the transmitting antenna respectively.
- the phase of the two transmitted signals arriving at the receiving antenna is also 180° out of phase due to the difference in position from the receiving antenna, so that the two channels can cancel each other out.
- one of the transmitting antennas is used to generate a cancellation signal, thereby canceling the interference of the other transmitting antenna to the receiving antenna.
- the two transmitting antennas are replaced by the receiving antennas, and the receiving antennas are replaced by the transmitting antennas.
- the function of the power splitter at this time is power combining, and the obtained two receiving ones are obtained (two Receiving antenna and one transmitting antenna)
- the principle of the antenna system is the same as that of the literature, such as an error! Reference source not found. Shown.
- the scheme shown in Figures 1 and 2 uses an auxiliary antenna to generate an interference cancellation signal, increasing the number of antennas.
- Another prior art solution is to increase the distance between the transmitting and receiving antennas.
- the increase in antenna distance can increase the free space loss of interference, thereby increasing the isolation between the transmitting and receiving antennas.
- the increase in antenna distance makes the size of the entire antenna system larger. Summary of the invention
- the present invention provides an antenna system which simplifies the number of antennas of an antenna system and an example between antennas.
- a first aspect of the present invention provides an antenna system, which may include: a transmitting antenna, a receiving antenna, a radome above the transmitting antenna and the receiving antenna, and a reflector located in the radome, The signal received by the transmitting antenna is reflected by the reflector and the signal received by the receiving antenna and the same-frequency interference signal generated by the transmitting antenna directly received by the receiving antenna cancel each other.
- the distance from the transmitting antenna to the incident point of the reflector is A, and the receiving antenna is to the reflector
- the distance from the incident point is / 2
- the distance from the transmitting antenna to the receiving antenna is D
- the reflection coefficient of the reflector is ⁇
- the transmitting signal of the transmitting antenna is reflected by the reflector
- the phase of the signal received by the receiving antenna and the transmitting signal of the transmitting antenna are directly received by the receiving antenna, then:
- ⁇ is the carrier wavelength and ⁇ is the phase of the reflection coefficient ⁇ .
- a reflection coefficient of the reflector is ⁇ , where ⁇ is an incident carrier angle of the transmitting antenna to the reflector; And the receiving antenna is configured to receive a carrier angle of a signal reflected by the reflector; ⁇ is a carrier angle of a co-channel interference signal generated by the transmitting antenna to the receiving antenna; and is used by the receiving antenna Receiving a carrier angle of the co-channel interference signal generated by the transmitting antenna, and the amplitude of the signal received by the receiving antenna after the transmitting signal of the transmitting antenna is reflected by the reflector is G t , ⁇ , f) PLi , ⁇ ].
- PIJ , ⁇ 2 ⁇ , ⁇ , f) the amplitude of the co-channel interference signal generated by the transmitting antenna of the transmitting antenna directly received by the receiving antenna is
- / is the carrier frequency
- M is the amplitude of the reflection coefficient r
- G 6 ⁇ , , /) is the emission
- the gain of the antenna to the reflector transmitting carrier, ⁇ is the carrier gain of the receiving carrier for receiving the reflected carrier of the reflector, ⁇ ( ⁇ , , ) is the transmitting signal of the transmitting antenna is directly received by the receiving antenna
- the transmit carrier gain of the co-channel interference signal generated, G R ( ⁇ , , ) is the carrier gain of the same-frequency interference signal generated by the receiving antenna for receiving the transmitting antenna, PL(f, l x )
- the corpse (/, / 2 ) are the path loss of the transmitting antenna to the reflector and the path loss of the reflector to the receiving antenna, respectively, D) the path of the transmitting antenna to the receiving antenna loss.
- the reflector is a single dielectric constant medium.
- the reflector is a conductor.
- the reflector is formed by laminating dielectrics of different dielectric constants.
- the reflector includes a plurality of media having different dielectric constants, and the plurality of media The Y-axis direction is discretely arranged in the XYZ three-dimensional coordinates.
- the reflector is completely embedded in the radome
- the reflector is partially embedded in the radome
- the reflector is fixed to an inner surface of the radome.
- the antenna system includes: a transmitting antenna, a receiving antenna, a radome above the transmitting antenna and the receiving antenna, and a reflector located in the radome, a signal received by the transmitting antenna and reflected by the reflector is received by the receiving antenna and a transmitting signal of the transmitting antenna is directly received by the receiving antenna
- the generated co-channel interference signals cancel each other out. Therefore, the embodiment of the present invention can implement the cancellation of the same-frequency interference signal of the transmitting antenna to the receiving antenna without additionally increasing the number of antennas and increasing the distance of the antenna.
- FIG. 1 is a schematic structural diagram of an embodiment of a prior art antenna system
- FIG. 2 is a schematic structural diagram of another embodiment of a prior art antenna system
- FIG. 3 is a schematic structural diagram of an embodiment of an antenna system according to the present invention.
- FIG. 4 is a schematic diagram of a reflection principle of an antenna system according to the present invention.
- Figure 5 is a schematic view showing the distribution of an embodiment of the reflector of the present invention.
- FIG. 6 is a schematic view showing the distribution of another embodiment of the reflector of the present invention.
- FIG. 7 is a schematic structural diagram of another embodiment of an antenna system according to the present invention.
- FIG. 8 is a schematic view showing the positional relationship between a reflector and a radome according to an embodiment of the present invention. Specific embodiment
- FIG. 3 is a schematic structural diagram of an embodiment of an antenna system according to the present invention.
- the antenna system of the embodiment of the present invention may include: a transmitting antenna 10, a receiving antenna 20, a radome 30 located above the transmitting antenna 10 and the receiving antenna 20, and the antenna
- the co-channel interference signals i.e., the co-channel interference signals of the transmitting antenna 10 to the receiving antenna 20
- the co-channel interference signals i.e., the co-channel interference signals of the transmitting antenna 10 to the receiving antenna 20
- the signal received by the transmitting antenna 10 and reflected by the receiving antenna 20 and the transmitting signal of the transmitting antenna 10 are directly transmitted by the receiving antenna 20
- the received co-channel interference signals cancel each other specifically: the amplitude of the signal received by the receiving antenna 20 and the transmission of the transmitting antenna 10 after the transmitting signal of the transmitting antenna 10 is reflected by the reflector 40
- the shape of the radome is any feasible shape, such as a plane, a paraboloid, a sphere, and the like.
- FIG. 4 is a schematic diagram of a signal transmission principle of the antenna system of the present invention.
- the reflection and transmission of the transmitted signal carrier of the transmitting antenna 10 are performed in a total of four layers of dielectric regions. From bottom to top are: air layer (dielectric constant), reflector layer (dielectric constant), radome material layer (dielectric constant A) and air layer (dielectric constant). error!
- the reference source was not found.
- the direction of the main lobe of the antenna is parallel to the normal direction of the interface of the reflector.
- the projection point of the transmitted signal on the reflector is at the intersection of the intersection of the line between the transmitting antenna 10 and the receiving antenna 20 and the interface of the reflector 40.
- the gains of the transmitting antenna 10 and the receiving antenna 20 be ⁇ ⁇ ( ) and ⁇ ⁇ ( ⁇ , respectively, which are the antenna operating frequency / and the spherical coordinates (the angle between the carrier and the Z-axis in the spherical coordinates) and (for the carrier The function is to measure the angle formed by the X and Y axes in the spherical coordinates, and the angle formed by the X axis.
- phase change amount ⁇ and the signal of the signal formed by the transmitting antenna 10 reflected by the reflector 40 to the receiving antenna 20 are The relationship between the phase change amount ⁇ % of the same-frequency dry 4 signal generated by the transmitting antenna 10 to the receiving antenna 20 satisfies:
- the transmission carrier angle of the transmitting antenna 10 to the reflector 40 is set (in conjunction with FIG. 4, assuming that the transmitting antenna 10 is incident on the reflector 40 in the direction of the transmitting carrier ⁇ of the reflector 40, the sum may be respectively It is the sum of ⁇ in Figure 4, where is the angle between / and the axis, ⁇ is the angle between A and the plane of the X and Y axes and the X axis, that is, specifically between the X and Y axes in Figure 4.
- the angle between the dotted line and the X-axis; the receiving carrier antenna 20 is used to receive the received carrier angle of the reflected signal of the reflector 40; ⁇ , the same-frequency interference signal generated by the transmitting antenna to the receiving antenna The carrier angle of the carrier antenna is used to receive the received carrier angle of the co-channel interference signal of the transmitting antenna 10.
- the amplitude of the signal received by the receiving antenna and the transmitting signal after the transmitting signal of the transmitting antenna is reflected by the reflector and the transmitting
- the amplitude of the co-channel interference signal generated by the transmitting signal of the antenna directly received by the receiving antenna needs to be equal, which specifically satisfies:
- ⁇ (O , /) is the gain of the transmitting carrier 10 to the transmitting carrier of the reflector 40
- ( ⁇ ( , , /) is the gain of the receiving antenna 20 for receiving the reflected carrier of the reflector 40
- G ⁇ 2 , / is the gain in the direction of the co-channel interference signal generated by the transmitting antenna 10 to the receiving antenna 20, and ( ⁇ , /) is the gain of the receiving antenna 20 for receiving the same-frequency interference, PL ⁇ , ! and corpse (/, / 2 ) are the path loss of the transmitting antenna 10 to the reflector 40 and the reflector, respectively
- the path loss of 40 to the receiving antenna 20, ⁇ (/, ⁇ )), is the interference path loss of the transmitting antenna 10 to the receiving antenna 20.
- G T , f , - PL , f , ⁇ ) ⁇ G R (pK f, ( 5 ) is known from the formula (3).
- the embodiment of the present invention adjusts the reflector 40 and the transmitting antenna.
- the positional relationship between the 10 and the receiving antenna 20 (i.e., adjustment, / 2 and D) can achieve phase cancellation of the co-channel interference signal.
- the offset of the amplitude of the co-channel interference signal can be achieved by selecting the reflector 40 having the appropriate reflection coefficient ( (ie, selecting the appropriate one).
- the calculation method of the reflection coefficient is a prior art, and will not be described in detail in the present invention.
- the reflector is a single dielectric constant medium.
- the distance from the transmitting antenna 10 to the incident point of the reflector 40 is the distance from the transmitting antenna to the incident point of the single dielectric constant medium.
- the distance from the receiving antenna 20 to the reflector 40 is the distance from the receiving antenna to the incident point of the single dielectric constant medium.
- the reflector is a conductor.
- the distance from the transmitting antenna 10 to the incident point of the reflector 40 is the distance from the transmitting antenna to the incident point of the conductor.
- the distance from the receiving antenna 20 to the reflector 40 is the distance from the receiving antenna to the incident point of the conductor.
- the reflector 40 in order to obtain the enthalpy values satisfying the requirements of the formulas (3) and (5), the reflector 40 may be laminated by a medium having different dielectric constants, as shown in FIG. In some feasible embodiments, in order to satisfy the phase relationship of the formula (3) and the magnitude relationship of the formula (5), the reflector 40 may be formed using a plurality of media arranged in a discrete manner, as shown in FIG. In the middle, the discrete direction may be selected as the Y-axis, that is, the reflector 40 includes a plurality of media, and the plurality of media are discretely arranged in the Y-axis direction in the XYZ three-dimensional coordinates.
- the dielectric constants of the plurality of media of the reflector 40 may be the same or different; each of the plurality of media may be a single layer medium, may be a conductor or a multilayer medium; Each of the plurality of media may be completely embedded in the radome, or partially embedded in the radome, or fixed to an inner surface of the radome.
- incident points for example, on the X-axis.
- the direction further includes a portion of the medium, the phase change amount generated when the carrier wave transmitted by the transmitting antenna 10 is incident on the medium of the reflector 40 and received by the receiving antenna 20, and the transmitting antenna 10
- the reflector dielectric constant can be less than or greater than the dielectric constant of the radome.
- the reflector in the embodiment of the present invention may also be a plurality of spatially discretely distributed reflectors. Adjusting the placement position of the reflector, the amount of phase change generated when the carrier transmitted by the transmitting antenna is incident on the reflectors and received by the receiving antenna after multiple reflections, and the transmitting antenna is received by the transmitting antenna The difference in the amount of phase change of the antenna interference can still be satisfied.
- FIG. 7 shows that three reflectors (respectively having a dielectric constant of 41)
- the reflector 42 having a dielectric constant is a reflector 43 having a dielectric constant of ⁇ 4 to eliminate the same-frequency interference signal.
- the dielectric constants of the selected reflectors may be the same or different.
- the reflector may be completely embedded in the radome ((a) in FIG. 8); or, the reflector is partially embedded in the radome Medium ((b) in Fig. 8); or, the reflector is fixed to the inner surface of the radome ((c) in Fig. 8).
- the reflector 40 in Fig. 8 can also be replaced with any one of the reflector 41, the reflector 42, and the reflector 43.
- the transmit and receive antennas of the present invention may be directional antennas and omnidirectional antennas.
- the present invention cover the modifications and variations of the inventions
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Abstract
本发明涉及通信领域,特别涉及一种天线***,其包括:一个发射天线、一个接收天线,位于所述发射天线和所述接收天线上方的天线罩,以及位于所述天线罩内的反射体,所述发射天线的发射信号经所述反射体反射后被所述接收天线接收到的信号与所述发射天线的发射信号直接被所述接收天线接收到而产生的同频干扰信号互相抵消。由此,本发明实施例可在不额外增加天线数量以及增大天线距离的情形下,实现发射天线对接收天线的同频干扰信号的消除。
Description
一种天线*** 技术领域
本发明涉及通信领域, 特别涉及一种天线***。 背景技术
微波通信设备通常采用不同的频率同时发送和接收信号, 这种频谱利用方 式造成了频谱资源的浪费。 由此产生的全双工通信技术, 即在同一段频谱上进 行数据发送的同时, 也进行数据接收的频谱利用方式, 能极大地提升频谱的利 用效率。
全双工通信中的一个关键问题是, 由于设备发射和接收同频, 设备的发射 天线会对本端接收天线产生同频干扰, 而且同频干扰不能使用滤波器抑制。 因 此, 提升设备收发天线之间的隔离度是实现全双工通信需要解决的一个关键问 题。
目前有以下两种现有技术解决全双工通信技术下的设备收发天线之间的同 频干扰问题。
图 1和图 2为现有技术中采用三天线的技术方案。 如错误! 未找到引用源。 所示, 该技术方案使用两个发射天线 TX1和 TX2以及一个接收天线 RX。 两发 射天线与接收天线的距离之差为 '2 ,其中 为载波的波长。发射天线 TX1和 TX2 发射的信号被接收天线 RX接收到, 从而产生同频干扰。
在方案中, 发射信号被功率分配器分成两路相同的信号分别馈入发射天线
TX1和 TX2中, 由于距离接收天线的位置相差 则到达接收天线处的两路发 射信号的相位也相差 180° , 从而两路干扰能相互抵消。
该技术方案中, 其中一个发射天线的作用是用来产生抵消信号, 从而将另 一个发射天线对接收天线的干扰抵消掉。
在该技术方案的基础上, 将两个发射天线用接收天线替换, 同时将接收天 线用发射天线替换,功率分配器此时的功能为功率合路,得到的 "两收一发"(两 个接收天线和一个发射天线) 天线***原理与文献技术方案相同, 如错误! 未 找到引用源。 所示。
图 1和图 2所示方案使用辅助天线产生干扰抵消信号, 增加了天线数量。 另一种现有技术方案是通过增大收发天线间的距离。 天线距离的增大能够 增大干扰的自由空间损耗, 从而增大收发天线间隔离度。 但是, 天线距离的增 大会使得整个天线***的尺寸变大。 发明内容
鉴于此, 本发明提供一种天线***, 可简化天线***的天线个数及天线之 间的举例。
本发明第一方面提供一种天线***, 其可包括: 一个发射天线、 一个接收 天线, 位于所述发射天线和所述接收天线上方的天线罩, 以及位于所述天线罩 内的反射体, 所述发射天线的发射信号经所述反射体反射后被所述接收天线接 收到的信号与所述发射天线的发射信号直接被所述接收天线接收到而产生的同 频干扰信号互相抵消。
结合第一方面, 在第一种可能的实现方式中, 所述发射天线的发射信号经 所述反射体反射后被所述接收天线接收到的信号与所述发射天线的发射信号直 接被所述接收天线接收到而产生的同频干扰信号互相抵消具体为: 所述发射天 线的发射信号经所述反射体反射后被所述接收天线接收到的信号的幅度与所述
发射天线的发射信号直接被所述接收天线接收到而产生的同频干扰信号的幅度 相等, 相位相差 (2" + \)π,η = 0,±1,±2,…。
结合第一方面的第一种可能的实现方式, 在第二种可能的实现方式中, 所 述发射天线到所述反射体的入射点的距离为 A , 所述接收天线到所述反射体的 入射点的距离为 /2, 所述发射天线到所述接收天线的距离为 D,所述反射体的 反射系数为 Γ , 则所述发射天线的发射信号经所述反射体反射后被所述接收 天线接收到的信号的相位与所述发射天线的发射信号直接被所述接收天线接收 到而 , 则:
其中, λ为载波波长, ^为反射系数 Γ的相位。
结合第一方面的第一种可能的实现方式, 在第三种可能的实现方式中, 所 述反射体的反射系数为 Γ , 、 ι 为所述发射天线到所述反射体的入射载波角 度; 、 为所述接收天线用于接收所述反射体所反射信号的载波角度; θ 、 为所述发射天线对所述接收天线产生的同频干扰信号的载波角度; 、 为 所述接收天线用于接收所述发射天线产生的同频干扰信号的载波角度, 则所述 发射天线的发射信号经所述反射体反射后被所述接收天线接收到的信号的幅度 为 Gt ,φ , f)' PLi ,ι^τ]. PIJ ,ι2γ ,φ^ , f),所述发射天线的发 射信号直接被所述接收天线接收到而产生的同频干扰信号的幅度为
GT、Θ ,φ , f、. PL、f ,D、 . , f、 ,
GT{e ^ PL{f x)-\T[PL{f 2)-GR{e^^ )=
GT(pT ,f、.Pl f,D、.GR(p^,f、
其中, /为载波频率, M为反射系数 r的幅度, G 6^, ,/)为所述发射
天线到所述反射体发射载波的增益, ^ 为所述接收天线用于接收反 射体的反射载波的载波增益, ^(^, , )为所述发射天线的发射信号直接被 所述接收天线接收到而产生的同频干扰信号的发射载波增益, GR (θ^ , , )为 所述接收天线用于接收所述发射天线产生的同频干扰信号的载波增益, PL(f, lx ) 和尸 (/,/2)分别为所述发射天线到所述反射体的路径损耗以及所述反射体到所 述接收天线的路径损耗, D)为所述发射天线到所述接收天线的路径损 耗。
结合第一方面至第一方面的第三种可能的实现方式中任一种, 在第四种可 能的实现方式中, 所述反射体为单介电常数的介质。
结合第一方面至第一方面的第三种可能的实现方式中任一种, 在第五种可 能的实现方式中, 所述反射体为导体。
结合第一方面至第一方面的第三种可能的实现方式中任一种, 在第六种可 能的实现方式中, 所述反射体由不同介电常数的介质层叠而成。
结合第一方面至第一方面的第三种可能的实现方式中任一种, 在第七种可 能的实现方式中, 所述反射体包括多个不同介电常数的介质, 所述多个介质在 XYZ三维坐标中的 Y轴方向离散排布。
结合第一方面至第一方面的第三种可能的实现方式中任一种, 在第八种可 能的实现方式中, 所述反射体完全嵌入到所述天线罩中;
或, 所述反射体部分嵌入到所述天线罩中;
或, 所述反射体固定在所述天线罩的内表面。
由上可见, 在本发明的一些可行的实施方式中, 天线***包括: 一个发射 天线、 一个接收天线, 位于所述发射天线和所述接收天线上方的天线罩, 以及
位于所述天线罩内的反射体, 所述发射天线的发射信号经所述反射体反射后被 所述接收天线接收到的信号与所述发射天线的发射信号直接被所述接收天线接 收到而产生的同频干扰信号互相抵消。 由此, 本发明实施例可在不额外增加天 线数量以及增大天线距离的情形下, 实现发射天线对接收天线的同频干扰信号 的消除。 附图说明
图 1为现有技术天线***一实施例的结构组成示意图;
图 2为现有技术天线***另一实施例的结构组成示意图;
图 3为本发明天线***一实施例的结构组成示意图;
图 4为本发明天线***的反射原理示意图;
图 5为本发明反射体一实施例的分布示意图;
图 6为本发明反射体另一实施例的分布示意图;
图 7为本发明天线***另一实施例的结构组成示意图;
图 8为本发明反射体与天线罩的一实施例的位置关系示意图。 具体实施例
下面通过具体的实施例对本发明进行详细说明。
图 3为本发明天线***一实施例的结构组成示意图。 如图 3所示, 本发明 实施例的天线***可包括: 一个发射天线 10, —个接收天线 20, 位于所述发射 天线 10和所述接收天线 20上方的天线罩 30,以及位于所述天线罩 30内的反射 体 40, 具体的, 所述发射天线 10的发射信号经所述反射体 40反射后被所述接 收天线 20接收到的信号与所述发射天线 10的发射信号直接被所述接收天线 20
接收到而产生的同频干扰信号(即发射天线 10对接收天线 20的同频干扰信号) 互相 4氐消。
在一些可行的实施方式中, 所述发射天线 10 的发射信号经所述反射体 40 反射后被所述接收天线 20接收到的信号与所述发射天线 10的发射信号直接被 所述接收天线 20接收到而产生的同频干扰信号互相抵消具体为: 所述发射天线 10的发射信号经所述反射体 40反射后被所述接收天线 20接收到的信号的幅度 与所述发射天线 10的发射信号直接被所述接收天线 20接收到而产生的同频干 扰信号的幅度相等, 相位相差 (2" + Ι)π, η = 0,±1,±2,…。
在一些可行的实施方式中, 所述天线罩的形状为任意可行的形状, 比如, 平面、 抛物面、 球面等。
进一步, 图 4为本发明的天线***的信号传输原理示意图。 如图 4所示, 发射天线 10的发射信号载波的反射和透射共在 4层介质区域中进行。 从下往上 依次为: 空气层(介电常数为 )、 反射体层(介电常数为 )、 天线罩材料层 (介电常数为 A )和空气层(介电常数为 )。 错误! 未找到引用源。 中以天线 的主瓣方向与反射体的分界面法线方向平行为例。 发射信号在反射体上的投射 点在发射天线 10和接收天线 20之间连线的中垂线与反射体 40的分界面的交点 处。 设发射天线 10和接收天线20的增益分别为<^( )和<^( ^, , 它们 是天线工作频率/和球坐标 (为载波与球坐标中 Z轴的夹角)和 (为载波 被映射到球坐标中的 X、 Y轴所在平面时, 与 X轴形成的夹角) 的函数。 具体 实现中,天线的增益可以通过测量得到。以天线主瓣朝向为 为例,从错误! 未找到引用源。 中可以看到, 能够使发射天线 10的载波投射到反射体 40上的 和 的取值为:
设电磁波在介质表面的反射系数为 Γ , 且令 T = \T\e]<p
其中, 1 1为反射系 数 Γ的幅度, 为反射系数 Γ的相位。 则发射天线 10的发射信号经反射体 40 反射后被接收天线 20接收到的信号相位变化为:
其中, /为载波频率; c为光速; 、 分别为发射天线 10和接收天线 20 到反射体 40的入射点的距离, 当入射点在发射天线 10和接收天线 20连线的中 垂线上时, 有 A =/2 = /。
接收天线 20接收到的同频干扰信号相对于发射天线 10处, 相位的变化量
=2^-·/·—
c (2) 其中 D为发射天线 10与接收天线 20之间的距离
为了满足发射天线 10对接收天线 20的同频干扰信号的相位能被抵消, 则 所述发射天线 10经所述反射体 40反射到所述接收天线 20所形成的信号的相位 变化量 Δ 和所述发射天线 10对所述接收天线 20产生的同频干 4尤信号的相位变 化量 Δ%之间的关系满足:
= (2η + \)·π η = 0,1,2,...
其中, λ为载波波长。 进一步,设 、 为所述发射天线 10到所述反射体 40的发射载波角度(结 合图 4, 假设发射天线 10到反射体 40的发射载波 Α的方向入射到反射体 40, 则 和 即可分别为图 4中的 和^ , 其中 为 /与 轴的夹角, ·为 A映 射到 X、 Y轴所在平面时与 X轴之间的夹角, 即 具体为图 4中 X、 Y轴之间 的虚线与 X轴之间的夹角); 、 为所述接收天线 20用于接收反射体 40反 射信号的接收载波角度; ^、 为所述发射天线对所述接收天线产生的同频干 扰信号的载波角度; ^、 为所述接收天线 20用于接收发射天线 10的同频干 扰信号的接收载波角度。
则为了满足发射天线 10对接收天线 20的同频干扰信号的幅度能被抵消, 所述发射天线的发射信号经所述反射体反射后被所述接收天线接收到的信号的 幅度与所述发射天线的发射信号直接被所述接收天线接收到而产生的同频干扰 信号的幅度需相等, 其具体满足:
PTX - GT {θ , φ , f) . PL{f, l, ) · |Γ| · PL{f, l2) - GR {Of, ^, f) =
PTX . GT、Θ ,φ , f、. PL f ,D). f、 ) 其中, Ptx为发射天线 lo 的功率; /为载波频率, M为反射系数 r的幅度,
<^(O ,/)为所述发射天线 10 到所述反射体 40 的发射载波的增益, (^ ( , ,/)为所述接收天线 20 用于接收反射体 40 反射载波的增益,
G θ2 ,/ 为所述发射天线 10对所述接收天线 20产生的同频干扰信号方向 上的增益,(^ ^^,/)为所述接收天线 20用于接收同频干扰的增益, PL{ ,! 和尸 (/,/2)分别为所述发射天线 10到所述反射体 40的路径损耗和所述反射体
40到所述接收天线 20的路径损耗, ^(/,^))为所述发射天线 10到所述接收 天线 20的干扰路径损耗。
GT , f、- PL、f ,Ό)· GR(pK f、 ( 5 ) 由式(3 )可知, 具体实现中, 本发明实施例通过调整反射体 40、 发射天线
10和接收天线 20三者之间的位置关系 (即调整 、 /2和 D ), 即可实现同频干扰 信号相位的抵消。
由式(5 )可知, 具体实现中, 在反射体 40、 发射天线 10和接收天线 20三 者之间的位置关系确定的情形下 (即式(5 ) 中除 之外的值均已确定), 本发 明实施例通过选择具有合适反射系数 Γ的反射体 40 (即选择合适的 ), 即可 实现同频干扰信号的幅度的抵消。 具体实现中, 反射系数的计算方法为已有技 术, 在本发明中不做详细描述。
在一些可行的实施方式中, 所述反射体为单介电常数的介质。 此时, 所述 发射天线 10到所述反射体 40的入射点的距离则为发射天线到该单介电常数介 质的入射点的距离。 以及, 所述接收天线 20到所述反射体 40的距离则为接收 天线到该单介电常数介质的入射点的距离。
在一些可行的实施方式中, 所述反射体为导体。 此时, 所述发射天线 10到 所述反射体 40的入射点的距离则为发射天线到该导体的入射点的距离。 以及, 所述接收天线 20到所述反射体 40的距离则为接收天线到该导体的入射点的距 离。
在一些可行的实施方式中, 为了获得满足式(3 )和式(5 )要求的 Γ值,所 述反射体 40可由不同介电常数的介质层叠而成, 如图 5所示。
在一些可行的实施方式中, 为满足式(3 )相位关系和式(5 ) 的幅度关系, 可使用离散排布的多个介质构成所述反射体 40, 如图 6所示的直角坐标系中, 可选择离散方向为 Y轴,即所述反射体 40包括多个介质,所述多个介质在 XYZ 三维坐标中的 Y轴方向离散排布。所述反射体 40的多个介质的介电常数可以相 同, 也可以不同; 所述的多个介质中每个介质可以是单层介质、 可以是导体也 可以是多层介质层叠而成; 所述的多个介质中, 每个介质可以完全嵌入到所述 天线罩中, 或者部分嵌入到所述天线罩中, 或者固定在所述天线罩的内表面。
在一些可行的实施方式中, 所述反射体 40上除了严格满足式(3 )和式(5 ) 的入射点之外, 如图 6所示, 还存在一些入射点 (比如, 在 X轴上的入射点), 所述发射天线 10发射的载波在所述发射体 40上的这些入射点反射后被所述接 收天线 20接收时产生的相位变化量 和所述发射天线 10对所述接收天线 20 干扰的相位变化量 Δ%之差接近 (2" + 1) τ, « = 0,±1,±2,· .. , 这对于干扰抵消也 是有帮助的。 所以所述反射体 40在 X方向上还包括一部分介质, 所述发射天线 10发射的载波入射到所述反射体 40的这些介质上反射后被所述接收天线 20接 收时产生的相位变化量 和所述发射天线 10对所述接收天线 20干 ·ί尤的相位变 化量 Δ%之差满足 (2" + 1 τ ± , " = 0,士 1,±2,…。 在一些可行的实施方式中, 本发明实施例中的反射体介电常数可小于或大 于天线罩的介电常数。
在一些可行的实施方式中, 本发明实施例中的反射体还可以是多个在空间 上离散分布的反射体。 适当调整反射体的放置位置, 所述发射天线发射的载波 入射到这些所述反射体上并经过多次反射后被所述接收天线接收时产生的相位 变化量和所述发射天线对所述接收天线干扰的相位变化量之差仍然可满足
(2" + 1 τ, " = 0,±1,±2,· . ·。 以及, 所述发射天线的发射信号经所述反射体反射 后被所述接收天线接收到的信号的幅度与所述发射天线的发射信号直接被所述 接收天线接收到而产生的同频干扰信号的幅度仍可相等。 比如, 图 7 示出了经 过三个反射体(分别为介电常数为 的反射体 41、 介电常数为 的反射体 42、 介电常数为 ε4的反射体 43、)的反射以消除同频干扰信号的实施例。具体实现中, 当采用多个反射体在空间上离散分布的方式来消除同频干扰信号时, 所选中的 反射体的介电常数可相同或者不同。
在一些可行的实施方式中, 如图 8 所示, 所述反射体可完全嵌入到所述天 线罩中 (图 8中的 (a ) ); 或, 所述反射体部分嵌入到所述天线罩中 (图 8中的 ( b ) ); 或, 所述反射体固定在所述天线罩的内表面 (图 8中的 (c ) )。 图 8 中 的反射体 40也可替换为反射体 41、 反射体 42以及反射体 43中任一种。
在一些可行的实施方式中, 本发明的发射天线和接收天线可为定向天线和 全向天线。 明的精神和范围。 这样, 倘若本发明的这些修改和变型属于本发明权利要求及 其等同技术的范围之内, 则本发明也意图包含这些改动和变型在内。
Claims
1、 一种天线***, 其特征在于, 包括: 一个发射天线、 一个接收天线, 位 于所述发射天线和所述接收天线上方的天线罩, 以及位于所述天线罩内的反射 体, 所述发射天线的发射信号经所述反射体反射后被所述接收天线接收到的信 号与所述发射天线的发射信号直接被所述接收天线接收到而产生的同频干扰信 号互相抵消。
2、 如权利要求 1所述的天线***, 其特征在于, 所述发射天线的发射信号 经所述反射体反射后被所述接收天线接收到的信号与所述发射天线的发射信号 直接被所述接收天线接收到而产生的同频干扰信号互相抵消具体为: 所述发射 天线的发射信号经所述反射体反射后被所述接收天线接收到的信号的幅度与所 述发射天线的发射信号直接被所述接收天线接收到而产生的同频干扰信号的幅 度相等, 相位相差 (2" + \)π, η = 0,±1,±2,…。
3、 如权利要求 2所述的天线***, 其特征在于, 所述发射天线到所述反射 体的入射点的距离为 A , 所述接收天线到所述反射体的入射点的距离为 /2 , 所 述发射天线到所述接收天线的距离为 D, 所述反射体的反射系数为 Γ , 则所 述发射天线的发射信号经所述反射体反射后被所述接收天线接收到的信号的相 位与所述发射天线的发射信号直接被所述接收天线接收到而产生的同频干扰信 号的 η = 0,1,2, . . .
其中, λ为载波波长, ^为反射系数 Γ的相位 (
4、 如权利要求 2所述的天线***, 其特征在于, 所述反射体的反射系数为 Γ , 、 为所述发射天线到所述反射体的入射载波角度; 、 ^为所述接 收天线用于接收所述反射体所反射信号的载波角度; 、 为所述发射天线对 所述接收天线产生的同频干扰信号的载波角度; 、 为所述接收天线用于接 收所述发射天线产生的同频干扰信号的载波角度, 则所述发射天线的发射信号 经所述反射体反射后被所述接收天线接收到 的信号的幅度为 GT (θ , ,/ PL(f, I, ) · |Γ| · /2 ) · GR (θ,κ ^ ), 所述发射天线的发射 信号直接被所述接收天线接收到而产生的同频干扰信号的幅度为 T、Θ ,φζ , f、. PL、f ,D、. GR{^ ,φ , f、 ,
其中, /为载波频率, lFl为反射系数 r的幅度, G 6^^'/)为所述发射 天线到所述反射体发射载波的增益, G 0^/)为所述接收天线用于接收反 射体的反射载波的载波增益, ^(^, , )为所述发射天线的发射信号直接被 所述接收天线接收到而产生的同频干扰信号的发射载波增益, GR (^,(^,f)为 所述接收天线用于接收所述发射天线产生的同频干扰信号的载波增益, PL{f, lx ) 和 PL、f, /2 )分别为所述发射天线到所述反射体的路径损耗以及所述反射体到所 述接收天线的路径损耗, D)为所述发射天线到所述接收天线的路径损 耗。
5、 如权利要求 1-4中任一项所述的天线***, 其特征在于, 所述反射体为 单介电常数的介质。
6、 如权利要求 1-4中任一项所述的天线***, 其特征在于, 所述反射体为 导体。
7、 如权利要求 1-4中任一项所述的天线***, 其特征在于, 所述反射体由 不同介电常数的介质层叠而成。
8、 如权利要求 1-4中任一项所述的天线***, 其特征在于, 所述反射体包 括多个不同介电常数的介质,所述多个介质在 XYZ三维坐标中的 Y轴方向离散 排布。
9、 如权利要求 1-4中任一项所述的天线***, 其特征在于,
所述反射体完全嵌入到所述天线罩中;
或, 所述反射体部分嵌入到所述天线罩中;
或, 所述反射体固定在所述天线罩的内表面。
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EP2940907A4 (en) | 2016-01-06 |
CN103392263B (zh) | 2016-03-30 |
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US9941585B2 (en) | 2018-04-10 |
EP2940907A1 (en) | 2015-11-04 |
US20150295308A1 (en) | 2015-10-15 |
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