Dual Band GNSS Antenna with High Back Lobe Suppression

Dual Band GNSS Antenna with High Back Lobe Suppression

Dual Band GNSS Antenna With High Back Lobe Suppression Sachit Varma, Stefano Caizzone Institute of Communication & Navigation, German Aerospace Center (DLR), Oberpfaffenhofen, Germany [email protected]; [email protected] Abstract—This paper presents the study of a novel design of a miniaturized GNSS antenna for E5a and E1 bands (i.e. at the central operating frequencies of 1.176 and 1.575 GHz) with high gain and very low back lobe for multipath reduction in high end static (e.g. geodesy) or dynamic (e.g. UAV) environments. The antenna itself is 56 mm in diameter and has a vertically stacked appurtenance of approximately 160 mm diameter that forces the cancellation of electromagnetic fields underneath the ground plane, thereby drastically improving the cross polariza- tion discrimination and allowing for multipath suppression in both bands of operation. Index Terms—antennas, cross polarization, GNSS, multipath, back lobe, interference. I. INTRODUCTION Fig. 1. Installed antenna with main and back lobe. The massive growth of GNSS (Global Navigation Satellite Systems) has been one of the biggest scientific and techno- the amount of multipath received. The paper is structured with logical achievements and has proven to be a global game the discussion of the the major performance metrics of the changer. What started in the early years as an elemental GNSS antenna, specifically related to multipath rejection, in development for providing the position, velocity and time to the beginning, followed by the current back lobe suppression support navigation and connectivity, has now evolved into a techniques. The design of the antenna comes next followed backbone technology for a plethora of innovative applications. by the proposed structure for high back lobe suppression. The Agriculture, racing, mountain sports, guidance of the visually simulation results are discussed next in detail, corresponding impaired, archaeology, geo-fencing, skydiving, atmospheric to the metrics defined, followed by some remarks to conclude sensing etc. are just a few of the areas that have immensely the possible future work associated with this technique. benefitted due to the outreach of GNSS [1], [2]. The variables II. ANTENNA PERFORMANCE METRICS in the picture are always the same, but making their use in life improving applications is what made GNSS a success. A. Cross Polarization Discrimination Like all other technologies based on electromagnetics, the GNSS antennas shall be designed to radiate in RHCP (Right robust and error-free use of GNSS comes with its share of Hand Circularly Polarized) mode and inhibit all kinds of challenges, namely interference, jamming and spoofing as the radiation in the LHCP (Left Hand Circularly Polarized) mode. major ones [3]. Any GNSS antenna, due to its non-ideal The ratio of the former to the latter exhibits the estimate of radiation characteristics, has a significant amount of back lobe the Cross Polarization Discrimination (XPD) over a specific radiation. This gives way for any signal being reflected from elevation beam angle, and this gives us the measure of how the surface of the platform, on which the antenna has been good can the antenna receive RHCP signals and mitigate installed, to be received by the antenna. This phenomenon, also LHCP signals. Although for detection, post-correlation and known as multipath, is one of the major contributing factors mitigation of multipath in urban scenarios, dual-polarized to errorneous GNSS measurement. As mentioned above, all operation, as discussed in [4] [5], is important to get a view of applications that involve the antenna being installed either the direction of the desired signals and the undesired multipath on a large ground plane (e.g. on unmanned aerial vehicles, signals, here in this paper the focus is on completely mitigating airplanes, satellites etc.) or on heterogeneous and irregular the undesired LHCP signals coming from the reflections below ground planes (e.g. on drones) pose a major problem since the ground plane. the antenna receives energy from its back lobe, e.g. as shown in Fig. 1. B. Front-to-Back Ratio This paper addresses this issue by proposing a structure The front-to-back ratio (FBR) of an antenna is one of below the radiating element, that would be able to minimize the most important metrics in applications where reflection underneath the ground plane severely hampers the received These cylindrical rings act as vertical cavities for electromag- signal quality and is defined as the ratio of the maximum netic cancellation of fields through resonance, thus giving rise power gain at the antenna boresight (i.e. at 0◦ elevation) to to standing waves. the maximum power gain at its opposite end (i.e. at 180◦ As elaborately studied in [13], [14] and well known in elevation) of the intended directional antenna, where the gain literature, in the transmission line model treatment of a at boresight refers to the RHCP signal gain and the gain at the metallic cavity, the incident voltage Vin, load voltage VL and negative side could refer to both RHCP or LHCP, whichever reflected voltage Vr in wave form can be given by: is higher in amplitude, as explained in [6]. In most cases, it is V (z; t) = V exp[j!(t − z=v)] the LHCP component which is stronger at 180◦ elevation, and in in the technique proposed in this paper would attempt to reduce Vr(z; t) = Vr exp[j!(t + z=v)] this value. 0 VL(z; t) = VL exp[j!(t − z=v )] C. Axial Ratio Factoring out the time dependence and applying the con- The axial ratio is the other important parameter of a ditons of voltage linearity and charge conservation at the circularly polarized antenna and is the ratio of the orthogonal junction, i.e. at z = 0, the reflection coefficient ρ would be: polarization fields of the antenna. For a perfectly circularly V Z − Z polarized antenna, the orthogonal components would be equal ρ = r = L 0 in magnitude and 90◦ apart in phase giving rise to an axial Vin ZL + Z0 ratio of 1 (or 0 dB) [7]. This ratio starts increasing in number The voltage and current as a function of transmission line as and when the antenna loses its perfect circular polarization length l can be given by: tendency and starts becoming elliptic, that happens at low V (l) = V exp(−j!l=v) + V exp(j!l=v) elevation angles for unoptimized antennas. The technique in r discussed in this would also attempt to improve the axial ratio I(l) = (Vin=Z0) exp(−j!l=v) − (Vr=Z0) exp(j!l=v) of the antenna at low elevation angles. Substituting these values for voltage and current, and for D. Multipath Suppression Indicator (MPSI) the angular frequency ! = 2πv/λ, solving for the line input As extensively analyzed and discussed in [8], in an impedance Z(l) = V (l)=I(l), we get: installed environment, the capability of the antenna istelf to ZL + jZ0 tan(2πl/λ) Z(l) = Z0 reject multipath signals is one of the key indicators of how Z0 + jZL tan(2πl/λ) well the overall system would perform in the presence of multiple and distinct sources of reflection. Different multipath If the termination is short circuited, i.e. at ZL = 0, Z(l) suppression indicators have been defined that would allow the would simply become: characterization of the standalone susceptibility of the antenna Z(l) = jZ0 tan(2πl/λ) to multipath for different scenarios of reflections (coming from below the antenna or from above via vertical and which gives rise to the fact that this short-circuited line slanted surfaces). This important information could then be would have infinite input impedance for transmission lengths used to predict the multipath and tune the antenna beforehand. equal to quarter of the operating wavelength, i.e. Z(l) = 1 for, l = (2n + 1)λ/4; where n 2 Z III. BACK LOBE SUPPRESSION FUNDAMENTALS & The study could be very easily made in terms of current as CURRENT TECHNIQUES well that is travelling on the inner cavity walls. The analogy In the context of reduced multipath coming from horizontal between this transmission line model and the cylindrical reflections from below the antenna horizon, there have been cavity is studied in [15] which shows that cavities with several techniques that work on mitigating this effect by conductor lengths equal to quarter wavelenghts would result targetting different electromagnetic characteristics of the an- in the voltages (or the electromagnetic currents) balancing tenna itself. Some of these techniques emphasize on reducing themselves out and causing standing waves. Horizontal choke the surface waves that radiate at low elevation angles at rings with such cavities have certain drawbacks such as their ground plane truncations as discussed in [9], but this leads bulky size and massive weight which makes installation on to deteriorated axial ratios since there isn’t any minimum small body platforms impossible. The other drawback is the radiation amplitude at these angles anymore. low gain at elevation angles beyond ±20◦ mostly due to low Studies on the effects of the ground plane on the antenna signal strength at these angles thereby causing deteriorated radiation characteristics has been studied in detail before [10] positioning accuracy as studied in [16]. and one of the most popular techniques involving horizontal Another concept to reduce the surface waves in planar choke rings have been developed [10], [11] and [12]. This antennas by introducing Electronic Band Gap (EBG) structures method is extremely common these days and involves choke has also been studied and developed [17]. Although the rings that are appended horizontally to the antenna structure. amount of back radiation is suppressed by this technique, the 0 330 10 30 RHCP without choke rings 0 LHCP without choke rings RHCP with choke rings 300 -10 60 LHCP with choke rings -20 -30 270 90 240 120 210 150 Fig.

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