Jim Hagerman 4/12/99

Similar documents
MERIS US Workshop. Instrument Characterization Overview. Steven Delwart

Requirements for the Star Tracker Parallel Science Programme

You, too, can make useful and beautiful astronomical images at Mees: Lesson 3

: Imaging Systems Laboratory II. Laboratory 6: The Polarization of Light April 16 & 18, 2002

Radiometry. Basics Extended Sources Blackbody Radiation Cos4 th power Lasers and lamps Throughput. ECE 5616 Curtis

A CubeSat Mission for Exoplanet Transit Detection and Astroseismology

AS750 Observational Astronomy

HICO Science Mission Overview

Chapter 4 Nadir looking UV measurement. Part-I: Theory and algorithm

First observations of the second solar spectrum with spatial resolution at the Lunette Jean Rösch

HICO Calibration and Atmospheric Correction

EXPOSURE TIME ESTIMATION

Capturing and Processing Planetary Images. Petros Pissias Eumetsat Astronomy Club 11/06/2015

PHOTOMETRIC EVALUATION AND CALIBRATION OF THE EARTHSHINE TELESCOPEE

Study of Physical Characteristics of High Apogee Space Debris

A Comparative Study and Intercalibration Between OSMI and SeaWiFS

X-ray imaging with amorphous selenium: Theoretical feasibility of the liquid crystal light valve for radiography

Single Emitter Detection with Fluorescence and Extinction Spectroscopy

A Stellar Gyroscope for CubeSat Attitude Determination

Ocean Optics XIV Conference, Kona, Hawaii 1998

= 6 (1/ nm) So what is probability of finding electron tunneled into a barrier 3 ev high?

11/5/12 Richard R. Auelmann. Low Light Imaging

Theoretical Examination

New Observation Results from A Rotating-drift-scan CCD System

The ALMA Optical Pointing Systems

OPTICAL PHOTOMETRY. Observational Astronomy (2011) 1

Radiometry. Nuno Vasconcelos UCSD

Photographing the Moon and the ISS. By Thierry Legault

What are Aerosols? Suspension of very small solid particles or liquid droplets Radii typically in the range of 10nm to

Astronomy 203 practice final examination

Optics.

Laboratory 3&4: Confocal Microscopy Imaging of Single-Emitter Fluorescence and Hanbury Brown and Twiss setup for Photon Antibunching

The URAT project August IAU GA Com. 8, Zacharias et al., the URAT project

Space Surveillance using Star Trackers. Part I: Simulations

Errors in Airglow & Auroral Emission Measurements

Brightness Calibration of Optical Spectrographs

Impacts of Atmospheric Corrections on Algal Bloom Detection Techniques

1 A photometric probe for Pan-STARRS

HICO OSU Website and Data Products

Laboratory 3: Confocal Microscopy Imaging of Single Emitter Fluorescence and Hanbury Brown, and Twiss Setup for Photon Antibunching

Comparison of Results Between the Miniature FASat-Bravo Ozone Mapping Detector (OMAD) and NASA s Total Ozone Mapping Spectrometer (TOMS)

2. To measure the emission lines in the hydrogen, helium and possibly other elemental spectra, and compare these to know values.

Confocal Microscopy Imaging of Single Emitter Fluorescence and Hanbury Brown and Twiss Photon Antibunching Setup

You should be able to demonstrate and show your understanding of:

Gemini Integration Time Calculators

Data Reduction - Optical / NIR Imaging. Chian-Chou Chen Ph319

홀로그램저장재료. National Creative Research Center for Active Plasmonics Applications Systems

Chandra was launched aboard Space Shuttle Columbia on July 23, 1999!!!

Coastal Characterization Using EO-1 Hyperion Data

AS 101: Day Lab #2 Summer Spectroscopy

Mandatory Assignment 2013 INF-GEO4310

Electro-Optical System. Analysis and Design. A Radiometry Perspective. Cornelius J. Willers SPIE PRESS. Bellingham, Washington USA

Reduction procedure of long-slit optical spectra. Astrophysical observatory of Asiago

Photometric Studies of GEO Debris

FLAT FIELDS FROM THE MOONLIT EARTH

ElectroMagnetic Radiation (EMR) Lecture 2-3 August 29 and 31, 2005

Pulsating White Dwarfs

Capturing and Processing Deep Space Images. Petros Pissias Eumetsat Astronomy Club 15/03/2018

CLOUD NOWCASTING: MOTION ANALYSIS OF ALL-SKY IMAGES USING VELOCITY FIELDS

Eight Years MOS-IRS Summary of Calibration Activities

Exploring Data. Keck LRIS spectra. Handbook of CCD Astronomy by Steve Howell Chap. 4, parts of 6

Radiometry HW Problems 1

Chapter 6 Telescopes: Portals of Discovery

DAY LABORATORY EXERCISE: SPECTROSCOPY

Auxiliaire d enseignement Nicolas Ayotte

Lab 5 The Green House Effect Pre-lab

*C. Pan 1, F. Weng 2, T. Beck 2 and S. Ding 3

Amateur Astronomer Participation in the TESS Exoplanet Mission

Transmission Electron Microscopy

Background The power radiated by a black body of temperature T, is given by the Stefan-Boltzmann Law

DISTRIBUTION LIST. Others original copies Name amount. Lens Research & Development 1x Uittenhout, J.M.M. 1x DOCUMENT CHANGE RECORD

CHALLENGES RELATED TO DETECTION OF THE LATENT PERIODICITY FOR SMALL-SIZED GEO DEBRIS

Spitzer Space Telescope

Analyzing Spiral Galaxies Observed in Near-Infrared

Landsat-8 Operational Land Imager (OLI) Initial On-Orbit Performance

optical / IR: photon counting flux density or magnitude corresponds to number of electrons per second (mean rate)

Lecture 2 Overview of Light in Water

* All those going out on the roof at night must carry a torch.

INAF-Osservatorio astrofisico di Torino Technical Report nr. 167

Imaging of vibrating objects using speckle subtraction

SOME ASPECTS OF PYROMETRY OF "WHITE" OBJECTS V.E.

Narrowband Imaging, or How to Image in Downtown Portland. Duncan Kitchin OMSI Astro Imaging Conference 2010

Lecture 9. PMTs and Laser Noise. Lecture 9. Photon Counting. Photomultiplier Tubes (PMTs) Laser Phase Noise. Relative Intensity

CSE 559A: Computer Vision EVERYONE needs to fill out survey.

Terahertz imaging using the Jefferson Lab - FEL high power broadband terahertz source

Plasma Spectroscopy in ISTTOK

Lecture Notes 2 Charge-Coupled Devices (CCDs) Part I. Basic CCD Operation CCD Image Sensor Architectures Static and Dynamic Analysis

Calibration of Ocean Colour Sensors

GCOM-C SGLI calibration and characterization. Hiroshi Murakami JAXA/EORC Satellite instrument pre- and post-launch calibration

UV Degradation of Polycarbonate

Refraction is the bending of light when it passes from one substance into another. Your eye uses refraction to focus light.

APPLICATION NOTE. Filter Set Prescription Alan Holmes

Comet Measurement Techniques. Karen Meech Institute for Astronomy Session 27 1/18/05

INTRODUCTION TO MICROWAVE REMOTE SENSING. Dr. A. Bhattacharya

Light Propagation in Free Space

Application Note Astronomy KITE, FALCON & OWL ASTRONOMY DATA August 2013, Northern Ireland

Ground and On-Orbit Characterization and Calibration of the Geosynchronous Imaging Fourier Transform Spectrometer (GIFTS)

Lab 1: Introduction to the sky and making telescopic observations with the CCD camera. AST 152M Lab Instructor: Greg Doppmann Due: Feb 11, 2000

WHAT PHOTOMETRIC PRECISION CAN I ACHIEVE? DAVID BOYD

1 The Preliminary Processing

Transcription:

This is an electro-optical analysis of the UCMS (underwater camera mapping system) designed for TerraSystems. Jim Hagerman 4/1/99 For simplicity the SNR of only one 5nm wide channel near 5nm is determined. The normal 6 fps mode (1/15s exposure) is used with an F/1.3 lens. Pixel sie is 9.9um on a side, so assume a capacity of about 8, electrons. Frame grabber is 1 bits, CCD quantum efficiency is about.44, and assume optics transmissivity of the lens to be about 8%. λ filter 5 ρ floor 1 F 1.3 x. pixel 9.9 1 6 y. pixel 9.9 1 6 τ optics.8 q e.44 t sample.8. 8 1 3 N 1, 1.. 1 λ 5. 1 9 h 6.63. 1 34 c 3. 1 8 d First we need to determine the noise of the camera. Dark current is specified as mv with a full scale output of 5mV at an ambient temperature of 6C. Since dark current doubles about every 7 degrees the noise at 4C ambient will be about 8 times less.. e dark 5. 8 e dark = 4 electrons per frame SNR of the camera is specified as 6dB. Ignoring dark current the read noise is simply e read 1 e read = 8 electrons Jerlov water characteristics are given by two coefficients, one for attenuation, and one for backscatter. The Jerlov 1B water type is clear coastal or better. a.5 b.11 K d a b n 1.33

Transmission of light through water is exponential as a function of depth. τ( ) e. K d Light from the sun is lost through the air-water interface (assuming ero angle) by τ surface. 4 n τ surface.98 = ( 1 n ) The backscattered light is a complex function of angle and depth. Using a simple model from Mobley that treats it as a lumped bulk component given by.33. b ρ ocean a ρ ocean =.7 Solar illumination of a bright sunny day at sea level is given as 1.5 watts per meter squared per nm. With a 5nm filter the illumination power per area is E sun. 1.5 λ filter The sterance (radiance) reflected off an object of maximum albedo (reflectance = 1) at depth is given by L floor ( ) E... sun ρ floor τ surface τ( ) π And the light power received by the detector at any given sled depth is Φ floor (, L..... floor ( ). π x pixel y pixel τ optics τ surface τ( 4. F Converting to CCD electrons per pixel per frame we get Φ.. floor (,. λ t sample q e. h c e floor ( 3, ) = 1.687 1 5

8 1 6 6 1 6 e floor (, 4 1 6 1 6 1 3 4 5 This is a lot of electrons and will saturate the detector if not stopped down. Nominally the sled is at a depth ( of near ero, just under the surface. The backscattered light is then approximated as a function of depth by L ocean ( ) E.. sun ρ ocean ( 1 τ( ) ) π Backscatter noise collected by the detector is Φ ocean (, d ) L..... ocean ( ). π x pixel y pixel τ optics τ surface τ( 4. F This converts to CCD electrons by e ocean (, Φ.. ocean (,. λ t sample q e. h c e ocean ( 3, ) = 4.47 1 5 At depths of 3m to 4m there is very little backscatter noise.

6 1 5 5 1 5 4 1 5 e ocean (, 3 1 5 1 5 1 1 5 1 3 4 5 The total number of electrons is the sum of signal, backscatter, and dark electrons. The aperture must be set such that the total does not saturate a pixel. e total (, e ocean (, e dark Aperture is calculated for a given camera depth as α( e total (, α( ) =.15 So at ero camera depth the worst case requires stopping down the lens by a factor of more than 6. At a depth of m the lens can be set wide open. This prevents pixel saturation. SNR is calculated taking into account aperture by

SNR(, α(. α(. e ocean (, d ) e dark e read. N 1 This formula assumes post processing to subtract out solar backscatter and dark signals. Thus, only the fluxuations of these noise sources remain. SNRs at various depths are plotted in the following graph for an object reflectivity of 1. In real life the reflectivies will be much lower. 15 SNR(, ) SNR(, 1) SNR(, ) SNR(, 3) 1 5 3 4 5 6 7 8 9 1