Crosswind Sniper System (CWINS)

Similar documents
Investigations on the performance of lidar measurements with different pulse shapes using a multi-channel Doppler lidar system

Understanding the performance of atmospheric free-space laser communications systems using coherent detection

Range Dependent Turbulence Characterization by Co-operating Coherent Doppler Lidar with Direct Detection Lidar

Bootstrap Beacon Creation for Dynamic Wavefront Compensation

Lab Report 3: Speckle Interferometry LIN PEI-YING, BAIG JOVERIA

A STUDY OF DOPPLER BEAM SWINGING USING AN IMAGING RADAR

Phased Array Velocity Sensor Operational Advantages and Data Analysis

SODAR- sonic detecting and ranging

Module 12 : System Degradation and Power Penalty

Active Radio Frequency Sensing for Soil Moisture Retrieval

Speckle Mitigation in Laser-Based Projectors

Nuove tecnologie per ecografia ad ultrasuoni: da 2D a 4D

Laser Speckle Reducer LSR-3000 Series

CHARA AO Calibration Process

Reference Distribution

Tracking of Moving Targets with MIMO Radar

Horizontal propagation deep turbulence test bed

Speckle free laser projection

between in the Multi-Gigabit Regime

LTE. Tester of laser range finders. Integrator Target slider. Transmitter channel. Receiver channel. Target slider Attenuator 2

1.6 Beam Wander vs. Image Jitter

Receiver Design for Passive Millimeter Wave (PMMW) Imaging

Diffuser / Homogenizer - diffractive optics

Dynamic Phase-Shifting Electronic Speckle Pattern Interferometer

Performance of the Prototype NLC RF Phase and Timing Distribution System *

Terahertz Wave Spectroscopy and Analysis Platform. Full Coverage of Applications From R&D to Industrial Testing

4GHz / 6GHz Radiation Measurement System

Wireless Channel Propagation Model Small-scale Fading

Optical Fiber. n 2. n 1. θ 2. θ 1. Critical Angle According to Snell s Law

NEXT-GENERATION ACOUSTIC WIND PROFILERS

SUPPLEMENTARY INFORMATION DOI: /NPHOTON

3.003 Lab 3 Part A. Measurement of Speed of Light

Spatially Resolved Backscatter Ceilometer

Wireless Power and Data Acquisition System for Large Detectors

Proposed Adaptive Optics system for Vainu Bappu Telescope

Department of Electrical Engineering and Computer Science

NOAA/OAR National Severe Storms Laboratory, Norman, Oklahoma

Principles of Modern Radar

In order to get an estimate of the magnitude limits of the CHARA Array, a spread sheet

Introduction. Learning Objectives. On completion of this class you will be able to. 1. Define fiber sensor. 2. List the different types fiber sensors

Atmospheric Compensation and Tracking Using Active Illumination

Bootstrap beacon creation for overcoming the. effects of beacon anisoplanitism in laser beam. projection system

DIFFERENTIAL ABSORPTION LIDAR FOR GREENHOUSE GAS MEASUREMENTS

Wavefront Sensing In Other Disciplines. 15 February 2003 Jerry Nelson, UCSC Wavefront Congress

PRELIMINARY STUDIES INTO THE REDUCTION OF DOME SEEING USING AIR CURTAINS

Principles of Pulse-Doppler Radar p. 1 Types of Doppler Radar p. 1 Definitions p. 5 Doppler Shift p. 5 Translation to Zero Intermediate Frequency p.

Determination of the correlation distance for spaced antennas on multipath HF links and implications for design of SIMO and MIMO systems.

THE NASA/JPL AIRBORNE SYNTHETIC APERTURE RADAR SYSTEM. Yunling Lou, Yunjin Kim, and Jakob van Zyl

Implementation of FSO Network under the Impact of Atmospheric Turbulences

200-GHz 8-µs LFM Optical Waveform Generation for High- Resolution Coherent Imaging

NEW LASER ULTRASONIC INTERFEROMETER FOR INDUSTRIAL APPLICATIONS B.Pouet and S.Breugnot Bossa Nova Technologies; Venice, CA, USA

Part Number SuperPix TM image sensor is one of SuperPix TM 2 Mega Digital image sensor series products. These series sensors have the same maximum ima

Development of a Low-order Adaptive Optics System at Udaipur Solar Observatory

Chemistry Instrumental Analysis Lecture 10. Chem 4631

Camera Calibration Certificate No: DMC III 27542

Fiber Optic Communication Link Design

A high resolution bunch arrival time monitor system for FLASH / XFEL

MAKING TRANSIENT ANTENNA MEASUREMENTS

(All-Fiber) Coherent Detection Lidars 2

Properties of Structured Light

Optical Correlator for Image Motion Compensation in the Focal Plane of a Satellite Camera

Lecture 10. Dielectric Waveguides and Optical Fibers

Australian Wind Profiler Network and Data Use in both Operational and Research Environments

Microwave Remote Sensing (1)

Optical Delay Line Application Note

Design of a Free Space Optical Communication Module for Small Satellites

MODULAR ADAPTIVE OPTICS TESTBED FOR THE NPOI

Scalable Front-End Digital Signal Processing for a Phased Array Radar Demonstrator. International Radar Symposium 2012 Warsaw, 24 May 2012

Terahertz Wave Spectroscopy and Analysis Platform. Full Coverage of Applications From R&D to Industrial Testing

Pixel-remapping waveguide addition to an internally sensed optical phased array

328 IMPROVING POLARIMETRIC RADAR PARAMETER ESTIMATES AND TARGET IDENTIFICATION : A COMPARISON OF DIFFERENT APPROACHES

A High-Resolution, Four-Band SAR Testbed with Real-Time Image Formation

Subject headings: turbulence -- atmospheric effects --techniques: interferometric -- techniques: image processing

Narrow line diode laser stacks for DPAL pumping

Ultrasound Beamforming and Image Formation. Jeremy J. Dahl

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

Implementation of a waveform recovery algorithm on FPGAs using a zonal method (Hudgin)

Optical Single Sideband Modulation and Optical Carrier Power Reduction and CATV Networks

The Impact of Very High Frequency Surface Reverberation on Coherent Acoustic Propagation and Modeling

Multi-Path Fading Channel

The Pierre Auger Observatory

Mobile System for Remote Sensing of Wind, Humidity, Temperature and Precipitation Microstructure Profiles during Special Events and Sport Competitions

Wave Sensing Radar and Wave Reconstruction

User s Guide Modulator Alignment Procedure

Sensors & Transducers Published by IFSA Publishing, S. L.,

The Radio Channel. COS 463: Wireless Networks Lecture 14 Kyle Jamieson. [Parts adapted from I. Darwazeh, A. Goldsmith, T. Rappaport, P.

CHAPTER 10 CONCLUSIONS AND FUTURE WORK 10.1 Conclusions

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

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

Exposure schedule for multiplexing holograms in photopolymer films

Multi aperture coherent imaging IMAGE testbed

MAORY E-ELT MCAO module project overview

Bias errors in PIV: the pixel locking effect revisited.

Information & Instructions

RADAR (RAdio Detection And Ranging)

SMART LASER SENSORS SIMPLIFY TIRE AND RUBBER INSPECTION

EARLY DEVELOPMENT IN SYNTHETIC APERTURE LIDAR SENSING FOR ON-DEMAND HIGH RESOLUTION IMAGING

Data sheet for TDS 10XX system THz Time Domain Spectrometer TDS 10XX

Channel effects on DSSS Rake receiver performance

Bistatic experiment with the UWB-CARABAS sensor - first results and prospects of future applications

Transcription:

Crosswind Sniper System (CWINS) Investigation of Algorithms and Proof of Concept Field Test 20 November 2006

Overview Requirements Analysis: Why Profile? How to Measure Crosswind? Key Principals of Measurement Algorithm Conceptual Descriptions 1A-G: Single Beam with Array Sampling Active using Gradient Measurements 1A-I: Single Beam with Array Sampling Active using Subaperture Intensity nsity Measurements 2A-I: Dual Beam or Dual Aperture Active using Full Aperture Intensity ty Measurements Candidate Algorithm Details Example Simulation Results Risk Reduction Analysis Link Budget Frozen Flow Hypothesis (Example Results from Earl Spillar) Proof of Concept Test Plan Path Forward 2

Why Profile? Average Cross Wind Velocity is sufficient only for constant wind case Wind Profiling yields significant targeting improvement for all other cases Drift (cm) Constant Velocity (10 mph) Uncorrected 1400 1200 1000 800 600 400 200 0 0 500 1000 1500 2000-200 Profile corrected -400-600 Range (M) Cumulative Wind Drift (cm) Zero Average Wind Profile [5, -5, 5, -5 mph] Uncorrected 50 40 30 20 10 0 0 500 1000 1500 2000-10 Profile corrected -20 Range (M) Cumulative Wind Drift (cm) Nonzero Average Wind Profile [7, -5, 5, 5 mph] Uncorrected Average Vel Corrected Profile corrected 100 80 60 40 20 0 0 500 1000 1500 2000-20 Range (M) Cumulative Wind Drift (cm) 500 400 300 200 100 Positive Variation Profile [10, 5, 0, 5] 0 0 500 1000 1500 2000-100 Profile corrected Range (M) Uncorrected Average Vel Corrected 3

Targeting Error Sources Effective at 2 Km Crosswind induced aimpoint error is the largest single error source 3D wind measurement may be required for precision targeting Targeting Error Sources (2 Km) 2 Km Target Error (cm) 1400 1200 1000 800 600 400 200 0 1253 cm Horizontal Displacement Uncompensated 10 mph Cross Wind 10 cm Horizontal Displacement Compensated 200 m segment 10 mph Cross Wind 500 cm Vertical Displacement Uncompensated 2 mph Vertical Wind 257 cm Vertical Displacement Uncompensated 10 mph Radial Wind 4

Measurement Algorithms Algorithms considered are variations on space-time auto-correlation 1A-G: Hartmann Lenslet Array (Gradient Pattern measurement at least a 2x2 or 4x4 array) 1A-I: Detector Array to measure (Intensity Pattern measurement at least a 2x2 or 4x4 array) 2A-I: Steer beam back and forth or use two detectors 2x2A-I: Steer beam in 2-d pattern or use 2x2 detectors Detector 1 Detector 2 5

Single Layer Measurement Procedure: N pulses transmitted Pulse #: 1 2... 3 N+1 N+2 N+3... N+2000 Backscattered pulses produce a 4 x 4 Intensity Pattern Pulse Intensity pattern pairs are cross-correlated Pairs are separated by N frames N selected for maximum correlation Pulse pairs yield a 7x7 Cross-Correlation pattern + + +... + = Cross-Correlation patterns averaged Wind Velocity Estimate = Identify Cross-Correlation peak Interpolation employed for resolution enhancement Peak Location Time for N pulses 6

Intensity Time Series (Range = 120 m) Method 2A-I Example Results Uniform Wind Evidence of correlation peaks at correct speed Longer range data corrupted by intensity variations in outgoing beam leads to correlation wash out Intensity fluctuations in the outgoing beam result in pulse-to-pulse variation of backscatter initial condition at the layer of interest. This variation increases with range and in turn reduces contrast in the space-time correlation function of the return beam. Detector 1 Detector 2 Delay compensated Time Series 120 m 360 m 600 m 840 m 1080 m Detector 1 Detector 2 7

Method 2A-I I Example Results 10% Wind Variation Along path Intensity Time Series (Range = 120 m) Poor 2A-I I correlation observed due to noise turbulence contributions from distinct velocity layers that wash out correlations 2A-I I correlation is further corrupted as the vertical component of wind increases Detector 1 Detector 2 Delay compensated Time Series 120 m 360 m 600 m 840 m 1080 m Detector 1 Detector 2 8

Profile Measurement Proof of Concept Simulation Example Simulation Example 1A-I algorithm with 4x4 sample 10 mph H wind 25% H/V random variation 5 velocity layers 120 m Center Range Truth Intensity Correlation Profiling 360 m Center Range Truth Intensity Correlation Profiling 600 m Center Range 840 m Center Range 1080 m Center Range Truth Truth Truth Intensity Correlation Profiling Intensity Correlation Profiling Intensity Correlation Profiling 1A-I I Algorithm exhibits < 10% 2D RMS velocity profile error 9

Top Level Algorithm Trades Method SNR 2D Measure? Ability to Profile Wind Relative Complexity 1A-G Must Reduce array size to 2x2 to get sufficient SNR Yes Good if using at least 4x4 Measurements High 1A-I Must Reduce array size to 2x2 or 4x4 to get sufficient SNR Yes Good if using at least 4x4 Measurements Modest 2A-I Full Aperture Improves SNR No Algorithm Definition more Difficult Modest 2x2A-I Full Aperture Improves SNR Yes Algorithm Definition more Difficult Modest 10

Link Budget Link Budget is challenging at 2 km Low visibility increases Mie scattering contribution, increasing SNR PARAMETER Transmit Pulse Energy = 20 J Visibility 23 km Visibility 10 km Visibility 4 km Visibility 23 km Visibility 10 km Visibility 4 km Range to Target (m) 2000.00 2000.00 2000.00 1600.00 1600.00 1600.00 Transmit Pulse Peak Power (dbm) with 6 ns pulse 68.00 68.00 68.00 68.00 68.00 68.00 Back-Scatter Contribution (db) -34.95-31.76-27.99-34.95-31.76-27.99 12.5 mm Aperture Collection Efficiency (db) -104.00-104.00-104.00-101.50-101.50-101.50 2 Way Transmission Loss (db) -0.77-1.71-4.23-0.60-1.37-3.40 Transmitter Optical Loss (db) -1.25-1.25-1.25-1.25-1.25-1.25 Receiver Optical Loss (db) -1.25-1.25-1.25-1.25-1.25-1.25 Total Received Power Per Subaperture (dbm) -74.21-71.97-70.72-71.55-69.13-67.39 Detector Sensitivity at 25 MHz (dbm) -63.00-63.00-63.00-63.00-63.00-63.00 Filter Gain (1 MHz Operation for Profiling - 15 MHz Operation for Range-Finding) (db) 6.99 6.99 6.99 6.99 6.99 6.99 SNR Required (db) -10.00-10.00-10.00-10.00-10.00-10.00 Speckle Noise (db) -0.07-0.05-0.03-0.12-0.09-0.05 Correlation gain from 2000 digital pulses averaging (db) 16.50 16.50 16.50 16.50 16.50 16.50 Link Margin(dB) 2.21 4.47 5.75 4.82 7.27 9.05 Total Measurement Time (Seconds) 1.00 1.00 1.00 1.00 1.00 1.00 11

Frozen Flow Hypothesis Turbulence Correlation Times For a vertical path the correlation time was measured to be long 100 to 500 msec For a horizontal path the correlation time was measured to be short 10 to 30 msec Weakly related to C 2 n SAIC captured data over a 1.3 km horizontal path directly over city using compact SRI AO system Terrain comparable to sniper engagement [Data from Spillar and Schoeck] 12

Proof of Concept Testbed 50mm x 50mm view space maps to 4x44 4 pixel space Pixels can be binned to simulate 2x2 and 4x4 arrays PC Interface & Control Card Lab LabView View M x M Detector Array Laptop Control Station Control Workstation Multiplexed ADC Collimating Lens Array Optical Sight Fiber Laser Collimated Laser Source Steering Mirror Backscatter Layer Post Processing Power Supply Pulse Generator Data Acquisition 13

Discussion / Path Forward Proof of concept simulation results establish feasibility Proof of concept test planned in immediate future Important remaining work (Future efforts): Complete SNR analysis including field measurement and noise statistics Develop improved algorithms exploiting 2x22 2 data 14