This invention relates to antennas and antenna radomes.
Global navigation satellite systems (GNSS) are widely used for high-precision positioning, such as the US Global Positioning System (GPS) and Russian global navigation system GLONASS, as well as some others. A GNSS antenna has to provide signal reception in the entire GNSS range, namely, a low-frequency band 1164-1300 MHz and a high-frequency band 1525-1610 MHz.
One of the most important positioning errors in GNSS systems is a so-called multipath error, when a signal reflected from the underlying ground surface appears at the input of the receiving antenna along with the line-of-sight signal.
The value of the multipath error is proportional to the ratio
This ratio is normally called the Down/Up ratio. In this ratio, θ is the elevation angle over the local horizon, and F(+l−θ) is the antenna pattern (AP) at angle θ above and under the local horizon (θ=0°) correspondingly. A spatial region where θ>0 is the upper or front hemisphere, otherwise, a spatial region at θ<0 is called the lower or backward hemisphere.
To provide a stable and reliable operation of positioning systems, quality signal reception from all satellites over the local horizon is required. The value F(θ) in the upper hemisphere should not vary highly. At the same time, the value F(θ) in the lower hemisphere should be as small as possible. So the value F(θ) should have a sharp drop in the vicinity of the local horizon (i.e., near θ=0°).
Receiving antennas thus need to provide such an AP whose level varies negligibly in the upper hemisphere, sharply drops when crossing the direction to the local horizon, and is small in the lower hemisphere. Also, such an antenna pattern needs to be provided over entire operational frequency range.
Accordingly, the present invention is directed to antenna radomes with cut-off patterns that substantially obviate one or more of the disadvantages of the related art.
An antenna system with a pattern whose level varies slightly in the upper hemisphere, drops in the direction of the local horizon, and is small in the lower hemisphere, over the entire desired frequency range. The antenna system includes a circularly-polarized antenna element placed inside a radome. The antenna element is to have a Down/Up ratio in a proximity of a local horizon of no better than −12 dB (The radome consists of some parts made from materials with different transparency. The basis of the proposed invention is a phenomenon of interference of the passed and diffractive fields in the shadow area, which has been formed by radome's semi-transparent surface. Due to using semi-transparent materials, one can control field interference, thereby shaping a desired antenna pattern for the proposed antenna system.
In another embodiment, there is provided an antenna system with a circularly-polarized antenna element with a Down/Up ratio in a proximity of a local horizon of no better than −12 dB, and an antenna radome providing a drop of antenna pattern near a local horizon and having transparent and semi-transparent areas, the transparent area being above the semi-transparent area. Optionally, the semi-transparent area contains multiple parts having different degrees of transparence. Optionally, each part of the semi-transparent area includes a set of slots with a specified impedance. Optionally, the semi-transparent area can comprise a set of vertical slots and a set of horizontal slots. Optionally, the radome includes a plurality of discrete elements providing the specified impedance. Optionally, the discrete elements include any of capacitors, inductors, resistors, connected in series and/or in parallel. Optionally, the semi-transparent area has a plurality of layers, each layer having a set of vertical slots and a set of horizontal slots.
In another embodiment, there is provided an antenna system includes a circularly-polarized antenna element with a Down/Up ratio in a proximity of a local horizon of no better than −12 dB, and an antenna radome enclosing the antenna element, the radome providing a drop of antenna pattern near a local horizon and having an upper transparent area and a lower semi-transparent area, The semi-transparent area is has a generally hemispherical shape, the semi-transparent area includes a circular metallized portion with vertical and horizontal slots, the metallized portion extending part of the way downward from an equator of the generally hemispherical shape, The metallized portion includes passive discrete elements connected across at least some of the slots. The metallized portion has a plurality of circular rows separated by the horizontal slots. Optionally, wherein the metallized portion includes multiple areas having different degrees of transparence. Optionally, each area of the metallized portion has a specified impedance. Optionally, the discrete elements include any of capacitors, inductors, resistors, connected in series and/or in parallel.
Additional features and advantages of the invention will be set forth in the description that follows, and in part will be apparent from the description, or may be learned by practice of the invention. The advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are intended to provide further explanation of the invention as claimed.
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention.
In the drawings:
Reference will now be made in detail to the preferred embodiments of the present invention, examples of which are illustrated in the accompanying drawings.
As shown in
The radome includes two segments—a semi-transparent segment 21 and transparent segment 22. The semi-transparent segment 21 is made of semi-transparent material. Semi-transparency here means the property of partial reflection and partial passing-through of electromagnet radiation. Numerical characteristics of such materials and a method of their implementation is given below. The transparent segment 22 is made of radio-transparent material, for example, thin dielectric with permeability close to 1. The transparent segment 22 is located above the semi-transparent one 21.
According to
A spherically shaped embodiment of the radome design is further described. A semi-transparent segment of the radome is a part of a sphere with radius R and center at point C. It includes two parts. The first part—211—is formed by an arc starting from the vertical axis and characterized by radius R and angle θ1. This part is made of nontransparent material that fully reflects or partly absorbs (with an angular dependency) electromagnetic radiation.
The second part of the semi-transparent segment 212 is formed by an arc of radius R, which starts at angle θ1 and ends at angle θ2. Angular dimension of the arc is θ2−θ1. Angle θ2 can take values greater than or equal to θ1. If the angles are the same, there is no semi-transparent surface in the design.
A transparent segment of the radome design 22 is located on an arc, which, together with the arcs of the semi-transparent segment 21, form a half of circle such that a sphere can be formed by rotating said arcs about the vertical axis. The segment is made of radio-transparent material. A criterion of referring to transparent, semi-transparent and nontransparent quality of a surface is given below.
Interaction of electromagnetic waves with semi-transparent surfaces can be characterized by a parameter called the layer impedance and designated by ZS. The impedance can be presented in the form of a sum ZS=RS+iXS, where RS, XS are active and reactive parts correspondingly. At XS>0 impedance is inductive. At XS<0, the impedance is capacitive. Components RS, XS are conveniently measured in relative units, fractions of the universal constant W0=120π Ohm (which is the free-space characteristic impedance). When |ZS|>>W0, the surface can be regarded as fully transparent. When |ZS|<<W0 the surface is regarded as nontransparent, fully reflecting electromagnetic waves similar to metals. When RS≠0, the surface partly absorbs electromagnetic waves. By selecting the desired layer impedance one can provide a required degree of passing electromagnetic radiation, its reflection and absorption, thereby affecting the interference mode of fields being passed-through and diffracted. When |ZS|˜W0, the surface is considered semi-transparent.
Antennas used in satellite positioning operate mainly in receiving mode, but in many cases it is practical to consider their characteristics in passing-through mode. The identity of antenna characteristics both in receiving and passing-through modes is proved by the reciprocity principle.
Calculations were done for a two-dimensional problem of diffracting a source field on a cylindrical surface of a certain radius R. The radiation of the source was assumed to be uniform in the range of angles ≥0, and in the range of θ<0 the radiation was suppressed. AP and Down/Up ratio for such a source are presented in
are given in
Radome design shown in
Both lumped and shared-circuit elements can be used as capacitors, resistors and inductors. Nominal values of these elements are selected based on the condition of suppressing field interference in the lower hemisphere at the required bandwidth.
The width of slots is defined by a convenient installation of elements containing resistors, inductors and capacitors. For example, for lumped elements the width of the slot is determined by the size of the corresponding components.
The semi-transparent area can include several layers. The structure of each layer corresponds to the structure of semi-transparent surfaces shown in
Below there are parameters of one radome embodiment, the use of which enable to reach DU(θ) ratio better than −20 dB starting from angle θ=12° in the lower hemisphere relative to the horizon.
R=2λ,θ1=0.52π,θ2=0.74π,ZS=−i0.5W0,
where R is the radius of the spherical radome, θ1, θ2 are the angles in terms of
Having thus described a preferred embodiment, it should be apparent to those skilled in the art that certain advantages of the described method and system have been achieved. It should also be appreciated that various modifications, adaptations, and alternative embodiments thereof may be made within the scope and spirit of the present invention. The invention is further defined by the following claims.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/RU2016/000251 | 4/27/2016 | WO | 00 |