Radar Signatures and Relations to Radar Cross Section. Mr P E R Galloway. Roke Manor Research Ltd, Romsey, Hampshire, United Kingdom

Similar documents
Non-Ideal Quiet Zone Effects on Compact Range Measurements

A NETWORK APPLICATION INTERFACE FOR RCS CALCULATIONS

A CYLINDRICAL NEAR-FIELD VS. SPHERICAL NEAR-FIELD ANTENNA TEST COMPARISON

DESIGN AND PERFORMANCE ANALYSIS OF A 1 40GHZ ULTRA-WIDEBAND ANTIPODAL VIVALDI ANTENNA

Accuracy Estimation of Microwave Holography from Planar Near-Field Measurements

Design of an Airborne SLAR Antenna at X-Band

Rec. ITU-R P RECOMMENDATION ITU-R P *

KULLIYYAH OF ENGINEERING

Tracking of Moving Targets with MIMO Radar

The Influence of Multipath on the Positioning Error

Detection of Multipath Propagation Effects in SAR-Tomography with MIMO Modes

DOPPLER RADAR. Doppler Velocities - The Doppler shift. if φ 0 = 0, then φ = 4π. where

ATCA Antenna Beam Patterns and Aperture Illumination

Antennas and Propagation. Chapter 4: Antenna Types

COMPARATIVE ANALYSIS BETWEEN CONICAL AND GAUSSIAN PROFILED HORN ANTENNAS

Keysight Technologies Pulsed Antenna Measurements Using PNA Network Analyzers

Enhancing space situational awareness using passive radar from space based emitters of opportunity

Continuous Arrays Page 1. Continuous Arrays. 1 One-dimensional Continuous Arrays. Figure 1: Continuous array N 1 AF = I m e jkz cos θ (1) m=0

CHAPTER 2 MICROSTRIP REFLECTARRAY ANTENNA AND PERFORMANCE EVALUATION

Physics B Waves and Sound Name: AP Review. Show your work:

PRIME FOCUS FEEDS FOR THE COMPACT RANGE

Lab 12 Microwave Optics.

Narrow- and wideband channels

Antenna Design and Site Planning Considerations for MIMO

Mobile Radio Propagation Channel Models

Microwave Remote Sensing (1)

Antenna Measurement Uncertainty Method for Measurements in Compact Antenna Test Ranges

Narrow- and wideband channels

DIGITAL BEAM-FORMING ANTENNA OPTIMIZATION FOR REFLECTOR BASED SPACE DEBRIS RADAR SYSTEM

REPORT ITU-R SA.2098

INTRODUCTION. Basic operating principle Tracking radars Techniques of target detection Examples of monopulse radar systems

Implementation of Orthogonal Frequency Coded SAW Devices Using Apodized Reflectors

Rec. ITU-R P RECOMMENDATION ITU-R P PROPAGATION BY DIFFRACTION. (Question ITU-R 202/3)

Introduction p. 1 Review of Radar Principles p. 1 Tracking Radars and the Evolution of Monopulse p. 3 A "Baseline" Monopulse Radar p.

DESIGN OF GLOBAL SAW RFID TAG DEVICES C. S. Hartmann, P. Brown, and J. Bellamy RF SAW, Inc., 900 Alpha Drive Ste 400, Richardson, TX, U.S.A.

Lecture 9. Radar Equation. Dr. Aamer Iqbal. Radar Signal Processing Dr. Aamer Iqbal Bhatti

Ultrasound Physics. History: Ultrasound 2/13/2019. Ultrasound

Multi-Path Fading Channel

A Stepped Frequency CW SAR for Lightweight UAV Operation

ELEC4604. RF Electronics. Experiment 1

Radar observables: Target range Target angles (azimuth & elevation) Target size (radar cross section) Target speed (Doppler) Target features (imaging)

MAKING TRANSIENT ANTENNA MEASUREMENTS

RECOMMENDATION ITU-R SA.1628

Set No.1. Code No: R

OVER TV SIGNALS. 1 Dpto. de Señales, Sistemas y Radiocomunicaciones. Universidad Politécnica

9. Microwaves. 9.1 Introduction. Safety consideration

RECOMMENDATION ITU-R F *

EENG473 Mobile Communications Module 3 : Week # (12) Mobile Radio Propagation: Small-Scale Path Loss

Aircraft Scatter on 10 and 24 GHz using JT65c and ISCAT-A

Channel. Muhammad Ali Jinnah University, Islamabad Campus, Pakistan. Multi-Path Fading. Dr. Noor M Khan EE, MAJU

CIRCULAR DUAL-POLARISED WIDEBAND ARRAYS FOR DIRECTION FINDING

The Design of an Automated, High-Accuracy Antenna Test Facility

Experiment 12: Microwaves

ECE 476/ECE 501C/CS Wireless Communication Systems Winter Lecture 6: Fading

Effects of snaking for a towed sonar array on an AUV

BROADBAND GAIN STANDARDS FOR WIRELESS MEASUREMENTS

Microwave Diffraction and Interference

GAIN COMPARISON MEASUREMENTS IN SPHERICAL NEAR-FIELD SCANNING

PHYS2090 OPTICAL PHYSICS Laboratory Microwaves

ECEN. Spectroscopy. Lab 8. copy. constituents HOMEWORK PR. Figure. 1. Layout of. of the

MOBILE RAPID-SCANNING X-BAND POLARIMETRIC (RaXPol) DOPPLER RADAR SYSTEM Andrew L. Pazmany 1 * and Howard B. Bluestein 2

2. Refraction and Reflection

Frequency-Modulated Continuous-Wave Radar (FM-CW Radar)

Design of a 915 MHz Patch Antenna with structure modification to increase bandwidth

A new Sensor for the detection of low-flying small targets and small boats in a cluttered environment

RECOMMENDATION ITU-R F.1819

A bluffer s guide to Radar

EEM.Ant. Antennas and Propagation

Chapter 41 Deep Space Station 13: Venus

Potential interference from spaceborne active sensors into radionavigation-satellite service receivers in the MHz band

Physics 476LW. Advanced Physics Laboratory - Microwave Optics

Effects on phased arrays radiation pattern due to phase error distribution in the phase shifter operation

INTRODUCTION TO RADAR SIGNAL PROCESSING

WIRELESS COMMUNICATION TECHNOLOGIES (16:332:546) LECTURE 5 SMALL SCALE FADING

This article reports on

Lecture 8. Radar Equation. Dr. Aamer Iqbal Bhatti. Radar Signal Processing. Dr. Aamer Iqbal Bhatti

A TECHNIQUE TO EVALUATE THE IMPACT OF FLEX CABLE PHASE INSTABILITY ON mm-wave PLANAR NEAR-FIELD MEASUREMENT ACCURACIES

Diffraction. Interference with more than 2 beams. Diffraction gratings. Diffraction by an aperture. Diffraction of a laser beam

Chapter 3 Solution to Problems

THE NATURE OF GROUND CLUTTER AFFECTING RADAR PERFORMANCE MOHAMMED J. AL SUMIADAEE

Channel Modelling ETIM10. Propagation mechanisms

Active Cancellation Algorithm for Radar Cross Section Reduction

A Broadband Reflectarray Using Phoenix Unit Cell

SEPTEMBER VOL. 38, NO. 9 ELECTRONIC DEFENSE SIMULTANEOUS SIGNAL ERRORS IN WIDEBAND IFM RECEIVERS WIDE, WIDER, WIDEST SYNTHETIC APERTURE ANTENNAS

HIGH ACCURACY CROSS-POLARIZATION MEASUREMENTS USING A SINGLE REFLECTOR COMPACT RANGE

CHAPTER 2 WIRELESS CHANNEL

WIDE SCANNING PHASED ARRAY ANTENNA USING PRINTED DIPOLE ANTENNAS WITH PARASITIC ELEMENT

ANTENNA INTRODUCTION / BASICS

Introduction to Radar Systems. The Radar Equation. MIT Lincoln Laboratory _P_1Y.ppt ODonnell

Newsletter 4.4. Antenna Magus version 4.4 released! Array synthesis reflective ground plane addition. July 2013

Introduction to Radar Systems. Radar Antennas. MIT Lincoln Laboratory. Radar Antennas - 1 PRH 6/18/02

Sensor and Simulation Notes. Note 505. December Development of the Impulse Slot Antenna (ISA) and Related Designs

Radiowave Propagation Prediction in a Wind Farm Environment and Wind Turbine Scattering Model

EC Transmission Lines And Waveguides

Broadband and High Efficiency Single-Layer Reflectarray Using Circular Ring Attached Two Sets of Phase-Delay Lines

Satellite TVRO G/T calculations

Modern radio techniques

ECE 476/ECE 501C/CS Wireless Communication Systems Winter Lecture 6: Fading

Active Radio Frequency Sensing for Soil Moisture Retrieval

CALIFORNIA STATE UNIVERSITY, NORTHRIDGE FADING CHANNEL CHARACTERIZATION AND MODELING

Transcription:

Radar Signatures and Relations to Radar Cross Section Mr P E R Galloway Roke Manor Research Ltd, Romsey, Hampshire, United Kingdom Philip.Galloway@roke.co.uk Abstract This paper addresses a number of effects that are often responsible for considerable differences between measured radar signatures and numerically predicted radar signatures. Numerical predictions are used to illustrate the likely magnitudes of these effects using two complex test targets. The paper comments on the potential pitfalls that can occur when measurements are made to validate predicted data. The fundamental problem is that for true validation, the prediction and measurement scenarios must be exactly aligned. The paper concludes that modern RCS prediction software is capable of generating reliable RCS data and that with care measurement procedures are possible that can generate suitable validation material. Introduction Roke Manor Research Ltd. (RMRL) has previously reported on the many applications of its RCS prediction software [1]. During the same conference, the German Company - Forschungsinstitut F r Hochfrequenzphysic (FGAN) also reported on a number of validation exercises conducted with two other RCS prediction codes []. The large differences reported provided the basis for an interesting investigation. This paper reports on some of the hypotheses generated by RMRL to explain the large differences. Geometry Quality The most obvious, but often missed issue, is that the CAD model used in the prediction must match very closely to the measured object. How close? As a starting point, the size and shape should have no areas that deviate from the object shape by more than one tenth of a wavelength at the highest prediction frequency. For predictions that only use high frequency techniques such as Physical Optics, Physical Theory of Diffraction, and Multiple Scattering techniques this is a sufficient criteria so long as the object has not been specifically designed to have an extremely low RCS. For Low Observable (LO) objects, greater care must be taken in geometry preparation and resonant region scattering mechanisms need to be included in the prediction process as these will start to introduce significant scattering contributions. Angular Sampling The selection of prediction parameters that provide sufficient sampling in angle is important. Numerical predictions have an inherently high precision in defining the angle of incidence of the illuminating wave onto a target. Figure 1 Sample Complex Target Geometry. Knott et al. [3] suggests that for a flat plate aperture of dimension L, the approximate value of the Null to Null beamwidth in degrees will be given by Equation 1.

θ 57 ( nul to nullbeamwidth) = Equation 1 λ L This criterion is for the main lobe width, whereas side lobes are generally half the main lobe angular width. To adequately sample a complex target an angle step size of the order of a sixth to an eighth of the value in Equation 1 will be needed. Overlay of Predictions for. Degree Step Size by. Degrees. The correlation is good, and it is not immediately clear that the envelope is not sufficiently sampled. Figure 3 Shows a similar overlay but with the offset set to.1-degrees. Here we see the initial match is good, but between ten and twenty degrees the apparent envelope of the prediction is completely different. 6 5.4 Degree Step Size 6 4 5 4 3 4 6 8 1 14 16 18. to. Degree Sweep. to. Degre Sweep Figure Closely spaced predictions. 6 5 4 3 Overlay for. Degree Step size with.1 Degree Offset 4 6 8 1 14 16 18.1 to.1 Degree Sweep. to. Degree Sweep Figure 3 Half stride offset predictions. To illustrate this the RCS of the object shown in Figure 1 was predicted at a range of angle step sizes. The target geometry is approximately ten meters wide and the predictions were performed at 5 GHz. From Equation 1 we see that the angular step size needs to be around.4 Degrees to give four samples per side lobe. Figure shows two predictions using a.- Degree step size but offset from each other 3 4 6 8 1 14 16 18 Sufficiently Sampled Signature Figure 4 Sufficiently sampled prediction. Figure 4 shows the same prediction sampled at.4 Degree steps, inline with the previously derived sampling requirement. This example shows that the criteria derived form Equation 1 is valid for this target. One interesting feature of the undersampled data is the tendency to capture the peak values of the envelope of the RCS, in the Degree region being around +dbsm. This tendency is due to the fact that in general nulls tend to be narrow in angular extent and the peaks in the lobes are wide in comparison. This example shows that structure of RCS plots can be misleading unless the sampling is sufficient. It also demonstrates that comparison of under sampled data will generally contain large (up to db) spot errors unless the angle sampling is controlled with great precision. If the object has significant multiple scattering interactions contributing to the signature then an even finer sampling in angle will generally be required to sufficiently capture the diffraction pattern. This is because the multiple scattering interactions generate an angular motion induced Doppler in excess of that expected from the physical extent of the target when imaged, which manifests as a larger effective equivalent aperture.

Measurement Considerations The previous section has shown that angular sampling and object alignment need to be precise for validation work. This is often not possible due to the mechanical limitations of the rotation apparatus. The quality of achievable rotator control and the effects of vibration from the environment can make fine sampling of angle resolution practically impossible for electrically large test objects. Near Field Criteria Knott et al. [3] provides a basic far field criteria for a target of principle dimension L and minimum range to the target R shown here in Equation. R L Equation λ It should be emphasised that this range criterion is derived from assumptions about a plane aperture that may not be valid for a complex target and will usually require a longer range. For targets with discrete scattering centres, that in isolation meet suitable far field criteria, it can be argued that the composite signature only changes a little when measured in the near field. Figure 5 Jeep Geometry Epsilon TM has the capability of predicting Radar Signatures (RS) by illuminating targets with a curved wave front as opposed to the RCS from standard plane wave. To illustrate the effects of wave curvature due to near field effects we present the following predictions. The target chosen for this is the jeep model that RMRL and FGAN have been working on. The object is about m wide and 4m long. The radar frequency for this example is GHz so the angle step size for this sweep is.5 Degrees. The far field criterion evaluates to approximately 1km. The near field prediction was performed at ten meters range and a five degree look down angle in elevation is used. RCS(RS) / dbsm 3 5 15 5-5 -15 Comparison of Near Field and Far Field predictions 9 95 5 1 Far Field RCS m Near Field RS Figure 6 Overlay of comparison predictions. Figure 6 shows an overlay of the near field and far field predictions. Over the 9-95 Degree region the difference is very large. This is probably due to the front grill of the jeep acting as an extended reflector. Clearly differences of db are possible from some classes of target structure. Over the remaining interval the near field signature is much the same as the far field one, supporting a discreet scattering centre hypothesis for the target at those angles. Wide Band Signatures The use of Spread spectrum or wide bandwidth signals has come to dominate mobile communications technology. Its use is also becoming widespread in Radar and navigation systems. This has generated the need to characterise radar signatures over substantial fractional bandwidths. It is known that for short pulse radar systems that a true RCS signature is not possible unless the pulse duration is at least twice the physical extent of the object it is interacting with. For wide bandwidth signatures similar steady

state requirements exist if RCS is to be used directly in the radar design process. Prediction technique Normal RCS prediction techniques evaluate the Bulk Signature at a spot frequency. If a number of evaluations are made at a series of spot frequencies then the frequency transfer function of the object can start to be approximated. Typical examples of wide band signatures include Range Profiles, Short Pulse Signature and microwave images. For the design of wide band radar systems it is important to know if predicted or measured bulk RCS figures are valid for link budget calculations. This will come down to the design of the radar waveform. In particular the transmitted bandwidth and the signal duration. Taking a range profile signature as an example, the unambiguous range available from the waveform needs to be larger than twice the principle dimension of the target L to allow for late time returns from multiple scattering features. It is also known that the bandwidth BW of the signal will determine the achievable resolution. Let T be the time taken to transmit the full signal bandwidth once (for pulse compression radars this would be the duration of the precompressed signal). We define T1 to be the dwell time of a single or equivalent single frequency component, and require that L T1 > Equation 3 c therefore T T.c N < T1 L = Equation 4 Where N is the equivalent number of steps of the frequency transfer function. To allow late time contributions to reach steady state and assuming that these will fall to a negligible level at twice the target length we require that the frequency step df should satisfy c df Equation 5 4L to provide sufficient unambiguous range. Therefore the bandwidth we transmit during time T should adhere to the following relationship to ensure unambiguous sampling of the target object. BW Tc NdF 8L = Equation 6 Generally care must be taken when using target bulk RCS figures for radar systems that break this relationship. Example In this example the target geometry of Figure 1 has been used. The prediction parameters were for a 36-Degree azimuth sweep at Degrees Elevation for a centre frequency of 5.5GHz and a 1GHz bandwidth. Figure 7 Range Profile vs Azimuth Map. Figure 7 Shows a range profile map covering a full 36-Degree sweep of the target. Figure 8 shows the transient Radar Signature (RS) synthesised for three different pulse lengths. For all the pulse widths there are a number of peak value transients in the signature. The 1m pulse never reaches steady state and generates a very Range Profile like plot. The m pulse also fails to reach a steady value. The 4m pulse has a long steady state region where the RS has converged to the Bulk RCS at the centre frequency of the sweep. Figure 9 shows a full 36-Degree azimuth sweep for the example target. A frequency average over the whole bandwidth is compared with the bulk RCS at the centre frequency. Note how the averaging tends to reduce the signature side-lobe peaks and generates a smooth signature.

Pulse Synthesis Plots RS / dbsm 5-5 -15-5 -3-35 -4-5 -4-3 3 4 5 Range / m 1m Pulse Width m Pulse Width 4m Pulse Width Figure 8 Pulse Synthesis at -Degree Azimuth for three pulse widths. Figure shows a comparison of the Frequency averaged data against a peakdetected signal for a -metre pulse length. Note how the peak-detected signal is generally higher than the frequency averaged plot. Figure 9 Frequency Average (dark) vs Centre Frequency Bulk signature (light) Polar Diagram. It is the intention of the author to extend the analysis capability to Epsilon TM to include integration under the received pulse, another common technique used in real radar systems. In general, pulse integration detection will operate much like the peak detection scheme so long as the steady state RS exceeds all the transient peaks. Figure Frequency Average (dark) vs Peak Detect Signature for m pulse length. Conclusions This paper has presented a number of ways to look at Radar Signatures and Radar Cross Section data for complex targets. Some of the pitfalls in comparing measured data to predicted data have been highlighted. In all cases the need to capture the data acquisition process, whether it be measurement or prediction is vital if comparisons are to be made. A number of methods of viewing wide bandwidth signatures have been presented and a criterion for the capture of wide bandwidth data has been suggested. References [1] Simpson S H W, Galloway P E R, Harman M, Applications of Epsilon TM A Radar Signature Prediction and Analysis Tool, International Radar Symposium IRS 98, Munich, Germany, September 1998. [] Biegel G., Essen H. at al., Validation of RCS Signature Simulations of Ground Targets at millimetre Wave Frequencies, Proceedings of IRS 98, Volume 1. pp413-4, Munich, September 1998. [3] Knott E F, Shaeffer J F, Tuley M T, Radar Cross Section, Second Edition, Artech House, 1993. ISBN -896-618-3