Modern Astronomical Optics 1
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Observation of the Airglow from the ISS by the IMAP Mission *Y
2013/3/13(ANGWIN workshop, Tachikawa) Observation of the airglow from the ISS by the IMAP mission *Y. Akiya [1], A. Saito [1], T. Sakanoi [2], Y. Hozumi [1], A. Yamazaki [3], Y. Otsuka [4] [1] Graduation School of Science, Kyoto University , [2] PPARC, Tohoku University, [3] ISAS/JAXA, [4] STE Laboratory, Nagoya University ----- Outline ----- Introduction of the IMAP mission Visible and near-infrared spectrographic imager Samples of airglow observation by VISI Summary “ISS-IMAP” mission Ionosphere, Mesosphere, Upper atmosphere and Plasmasphere Imagers of the ISS-IMAP mapping mission from the mission International Space Station (ISS) Observational imagers were installed on the Exposure Facility of Japanese Experimental Module: August 9th, 2012. Initial checkout: August and September, 2012 Nominal observations: October, 2012 - [Pictures: Courtesy of JAXA/NASA] [this issue]. According to characteristics of airglow emissions, wavelength range from 630 to 762 nm. Typical total intensity of such as intensity, emission height, background continuum, etc., we airglow is 100 1000 R as listed in Table 1, and 10 % variation of selected the airglow emissions which will be measured with VISI, the total intensity must be detected in order to investigate the and determined the requirements for instrumental design. The airglow variation pattern. In addition, short exposure cycle less targets and requirements are summarized in Table 1. than several seconds is necessary to measure small-scale airglow Table 1. Scientific Targets of VISI signatures (see Table 1) considering the orbital speed of ISS (~8 km/s). Airglow Required Region Scientific Typical A sectional view of VISI and its specifications are given in (waele- spatial (height) target intensity Figure 4 and Table 2, respectively. -
Hubble Space Telescope Primer for Cycle 25
January 2017 Hubble Space Telescope Primer for Cycle 25 An Introduction to the HST for Phase I Proposers 3700 San Martin Drive Baltimore, Maryland 21218 [email protected] Operated by the Association of Universities for Research in Astronomy, Inc., for the National Aeronautics and Space Administration How to Get Started For information about submitting a HST observing proposal, please begin at the Cycle 25 Announcement webpage at: http://www.stsci.edu/hst/proposing/docs/cycle25announce Procedures for submitting a Phase I proposal are available at: http://apst.stsci.edu/apt/external/help/roadmap1.html Technical documentation about the instruments are available in their respective handbooks, available at: http://www.stsci.edu/hst/HST_overview/documents Where to Get Help Contact the STScI Help Desk by sending a message to [email protected]. Voice mail may be left by calling 1-800-544-8125 (within the US only) or 410-338-1082. The HST Primer for Cycle 25 was edited by Susan Rose, Senior Technical Editor and contributions from many others at STScI, in particular John Debes, Ronald Downes, Linda Dressel, Andrew Fox, Norman Grogin, Katie Kaleida, Matt Lallo, Cristina Oliveira, Charles Proffitt, Tony Roman, Paule Sonnentrucker, Denise Taylor and Leonardo Ubeda. Send comments or corrections to: Hubble Space Telescope Division Space Telescope Science Institute 3700 San Martin Drive Baltimore, Maryland 21218 E-mail:[email protected] CHAPTER 1: Introduction In this chapter... 1.1 About this Document / 7 1.2 What’s New This Cycle / 7 1.3 Resources, Documentation and Tools / 8 1.4 STScI Help Desk / 12 1.1 About this Document The Hubble Space Telescope Primer for Cycle 25 is a companion document to the HST Call for Proposals1. -
Journal of Interdisciplinary Science Topics Determining Distance Or
Journal of Interdisciplinary Science Topics Determining Distance or Object Size from a Photograph Chuqiao Huang The Centre for Interdisciplinary Science, University of Leicester 19/02/2014 Abstract The purpose of this paper is to create an equation relating the distance and width of an object in a photograph to a constant when the conditions under which the photograph was taken are known. These conditions are the sensor size of the camera and the resolution and focal length of the picture. The paper will highlight when such an equation would be an accurate prediction of reality, and will conclude with an example calculation. Introduction may be expressed as a tan (opposite/adjacent) In addition to displaying visual information relationship: such as colour, texture, and shape, a photograph (1.0) may provide size and distance information on (1.1) subjects. The purpose of this paper is to develop such an equation from basic trigonometric principles when given certain parameters about the photo. Picture Angular Resolution With the image dimensions, we can make an Picture Field of View equation for one-dimensional angular resolution. First, we will determine an equation for the Since l2 describes sensor width and not height, we horizontal field of view of a photograph when given will calculate horizontal instead of vertical angular the focal length and width of the sensor. resolution: Consider the top down view of the camera (2.0) system below (figure 1), consisting of an object (left), lens (centre), and sensor (right). Let d be the (2.1) 1 distance of object to the lens, d2 be the focal length, Here, αhPixel is the average horizontal field of l1 be the width of the object, l2 be the width of the view for a single pixel, and nhPixel is the number of sensor, and α be the horizontal field of view of the pixels that make up a row of the picture. -
Sub-Airy Disk Angular Resolution with High Dynamic Range in the Near-Infrared A
EPJ Web of Conferences 16, 03002 (2011) DOI: 10.1051/epjconf/20111603002 C Owned by the authors, published by EDP Sciences, 2011 Sub-Airy disk angular resolution with high dynamic range in the near-infrared A. Richichi European Southern Observatory,Karl-Schwarzschildstr. 2, 85748 Garching, Germany Abstract. Lunar occultations (LO) are a simple and effective high angular resolution method, with minimum requirements in instrumentation and telescope time. They rely on the analysis of the diffraction fringes created by the lunar limb. The diffraction phenomen occurs in space, and as a result LO are highly insensitive to most of the degrading effects that limit the performance of traditional single telescope and long-baseline interferometric techniques used for direct detection of faint, close companions to bright stars. We present very recent results obtained with the technique of lunar occultations in the near-IR, showing the detection of companions with very high dynamic range as close as few milliarcseconds to the primary star. We discuss the potential improvements that could be made, to increase further the current performance. Of course, LO are fixed-time events applicable only to sources which happen to lie on the Moon’s apparent orbit. However, with the continuously increasing numbers of potential exoplanets and brown dwarfs beign discovered, the frequency of such events is not negligible. I will list some of the most favorable potential LO in the near future, to be observed from major observatories. 1. THE METHOD The geometry of a lunar occultation (LO) event is sketched in Figure 1. The lunar limb acts as a straight diffracting edge, moving across the source with an angular speed that is the product of the lunar motion vector VM and the cosine of the contact angle CA. -
[OI] 5577 in the Airglow and the Aurora
Journal of Resea rch of the National Bureau of Sta ndards- D. Radio Propagation Vol. 63D, No.1, July-August 1959 Origin of [OlJ 5577 in the Airglow and the Aurora Franklin E. Roach, James W. McCaulley, and Edward Marovich (January 30, 1959) The distribution of 5577 zenith intensities at stations in the subauroral zone iB found to be unimodal with no discontinuity at the visual threshold. This is interpreted as evi dence that 5577 airglow and 5577 aurora may have a common origin. 1. Introduction origin hypothesis, their critical characteristic being the lack of any discontinuity. It i cu tomary to refer to [01] 5577 as airglow if In figure 2, a replot of the histogram of St. Amand it is invisible and as aurora if it is visible. Thus, and Ashburn is shown with a regroupillg of the data the physiological visual threshold (at approximately to correspond to class intervals of 50 R rather than the 10 R that they used. They put an approxi 1,000 myleighs 1 for extended objects) has been assumed to have a physical significance in the upper mately normal curve through the plot on the basis atmosphere with different mechanisms operative of which they were able to state that an intensity above and below the threshold. The purpose of correspondulg to a just visible aurora should occur this paper is to inquil'e into the existence of a only "once or twice in geologic time." Because physical criterion to distinguish between 5577 auroras do occur occasionally, though rarely, in southern California, the implication is that an aurora airglow and 5577 aurora. -
The Most Important Equation in Astronomy! 50
The Most Important Equation in Astronomy! 50 There are many equations that astronomers use L to describe the physical world, but none is more R 1.22 important and fundamental to the research that we = conduct than the one to the left! You cannot design a D telescope, or a satellite sensor, without paying attention to the relationship that it describes. In optics, the best focused spot of light that a perfect lens with a circular aperture can make, limited by the diffraction of light. The diffraction pattern has a bright region in the center called the Airy Disk. The diameter of the Airy Disk is related to the wavelength of the illuminating light, L, and the size of the circular aperture (mirror, lens), given by D. When L and D are expressed in the same units (e.g. centimeters, meters), R will be in units of angular measure called radians ( 1 radian = 57.3 degrees). You cannot see details with your eye, with a camera, or with a telescope, that are smaller than the Airy Disk size for your particular optical system. The formula also says that larger telescopes (making D bigger) allow you to see much finer details. For example, compare the top image of the Apollo-15 landing area taken by the Japanese Kaguya Satellite (10 meters/pixel at 100 km orbit elevation: aperture = about 15cm ) with the lower image taken by the LRO satellite (0.5 meters/pixel at a 50km orbit elevation: aperture = ). The Apollo-15 Lunar Module (LM) can be seen by its 'horizontal shadow' near the center of the image. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
8. Adaptive Optics 299
8. Adaptive Optics 299 8.1 Introduction Adaptive Optics is absolutely essential for OWL, to concentrate the light for spectroscopy and imaging and to reach the diffraction limit on-axis or over an extended FoV. In this section we present a progressive implementation plan based on three generation of Adaptive Optics systems and, to the possible extent, the corresponding expected performance. The 1st generation AO − Single Conjugate, Ground Layer, and distributed Multi-object AO − is essentially based on Natural Guide Stars (NGSs) and makes use of the M6 Adaptive Mirror included in the Telescope optical path. The 2nd generation AO is also based on NGSs but includes a second deformable mirror (M5) conjugated at 7-8 km – Multi-Conjugate Adaptive Optics − or a post focus mirror conjugated to the telescope pupil with a much higher density of actuators -tweeter- in the case of EPICS. The 3rd generation AO makes use of single or multiple Laser Guide Stars, preferably Sodium LGSs, and should provide higher sky coverage, better Strehl ratio and correction at shorter wavelengths. More emphasis in the future will be given to the LGS assisted AO systems after having studied, simulated and demonstrated the feasibility of the proposed concepts. The performance presented for the AO systems is based on advances from today's technology in areas where we feel confident that such advances will occur (e.g. the sizes of the deformable mirrors). Even better performance could be achieved if other technologies advance at the same rate as in the past (e.g. the density of actuators for deformable mirrors). -
REMOTE SENSING of SEISMIC ACTIVITY on VENUS USING a SMALL SPACECRAFT: INITIAL MODELING RESULTS, A. Komjathy1, A. Didion1, B. Sutin1, B
49th Lunar and Planetary Science Conference 2018 (LPI Contrib. No. 2083) 1731.pdf REMOTE SENSING OF SEISMIC ACTIVITY ON VENUS USING A SMALL SPACECRAFT: INITIAL MODELING RESULTS, A. Komjathy1, A. Didion1, B. Sutin1, B. Nakazono1, A. Karp1, M. Wallace1, G. Lan- toine1, S. Krishnamoorthy1, M. Rud1, J. Cutts, J. Makela2, M. Grawe2, P. Lognonné3, B. Kenda3, M. Drilleau3 and Jörn Helbert4 1Jet Propulsion Laboratory, California Institute of Technology, USA 2University of Illinois at Urbana-Champaign, USA 3Institut de Physique du Globe-Paris Sorbonne, France 4Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany Introduction: The planetary evolution and struc- other at 4.3 µm (visible on the dayside). The signifi- ture of Venus remain uncertain more than half a centu- cant advantage of observing nightglow on Venus is ry after the first visit by a robotic spacecraft. To under- that it is much brighter on Venus than on Earth [2] and stand how Venus evolved it is necessary to detect the that airglow lifetime (~4,000 sec) is significantly long- signs of seismic activity. Due to the adverse surface er than the period of seismic waves (10-30 sec). This conditions on Venus, with extremely high temperature makes it very attractive for directly detecting surface and pressure, it is infeasible with current technology, waves on Venus. This is in sharp contrast with Earth even using flagship missions, to place seismometers on where the lifetime of airglow is about one order of the surface for an extended period of time. Due to dy- magnitude smaller (~110 sec) than, e.g., the tsunami namic coupling between the solid planet and the at- waves we routinely observe on Earth with 630 nm air- mosphere, the waves generated by quakes propagate glow instruments [4]. -
Understanding Resolution Diffraction and the Airy Disk, Dawes Limit & Rayleigh Criterion by Ed Zarenski [email protected]
Understanding Resolution Diffraction and The Airy Disk, Dawes Limit & Rayleigh Criterion by Ed Zarenski [email protected] These explanations of terms are based on my understanding and application of published data and measurement criteria with specific notation from the credited sources. Noted paragraphs are not necessarily quoted but may be summarized directly from the source stated. All information if not noted from a specific source is mine. I have attempted to be as clear and accurate as possible in my presentation of all the data and applications put forth here. Although this article utilizes much information from the sources noted, it represents my opinion and my understanding of optical theory. Any errors are mine. Comments and discussion are welcome. Clear Skies, and if not, Cloudy Nights. EdZ November 2003, Introduction: Diffraction and Resolution Common Diffraction Limit Criteria The Airy Disk Understanding Rayleigh and Dawes Limits Seeing a Black Space Between Components Affects of Magnitude and Color Affects of Central Obstruction Affect of Exit Pupil on Resolution Resolving Power Resolving Power in Extended Objects Extended Object Resolution Criteria Diffraction Fringes Interfere with Resolution Magnification is Necessary to See Acuity Determines Magnification Summary / Conclusions Credits 1 Introduction: Diffraction and Resolution All lenses or mirrors cause diffraction of light. Assuming a circular aperture, the image of a point source formed by the lens shows a small disk of light surrounded by a number of alternating dark and bright rings. This is known as the diffraction pattern or the Airy pattern. At the center of this pattern is the Airy disk. As the diameter of the aperture increases, the size of the Airy disk decreases. -
Subaru Super Deep Field (SSDF) with AO
Subaru Super Deep Field (SSDF) using Adaptive Optics Yosuke Minowa (NAOJ) on behalf of Yoshii, Y. (IoA, Univ. of Tokyo; PI) and SSDF team: Kobayashi, N. (IoA, Univ. of Tokyo), Totani, T. (Kyoto Univ.), Takami, H., Takato, N. Hayano, Y., Iye, M. (NAOJ). Subaru UM (1/30/2007) SSDF project: What? { Scientific motivation 1. Study the galaxy population at the unprecedented faint end (K’=23-25mag) to find any new population which may explain the missing counterpart to the extragalactic background light. 2. Study the morphological evolution of field galaxies in rest-frame optical wavelengths to find the origin of Hubble sequence. Æ high-resolution deep imaging of distant galaxies SSDF project: How? { Deep imaging of high-z galaxies with AO. z Improve detection sensitivity. Peak intensity: with AO ~ 10-20 times higher 0”.07 without AO z Improve spatial 0”.4 resolution FWHM < 0”.1 AO is best suited for the deep imaging study of high-z galaxies which requires both high-sensitivity and high-resolution. z SSDF project: Where? { Target field: a part of “Subaru Deep Field” (SDF) z Originally selected to locate near a bright star for AO observations (Maihara+01). z Optical~NIR deep imaging data are publicly available. { Enable the SED fitting of detected galaxies. Æ phot-z, rest-frame color, (Maihara+01) stellar mass… Observations { AO36+IRCS at Cassegrain z K’-band (2.12um) imaging with 58mas mode z providing 1x1 arcmin2 FOV AO36 IRCS To achieve unprecedented faint-end, we concentrated on K’-band imaging of this 1arcmin2 field, rather than wide-field or multi-color imaging. -
Nighttime Photochemical Model and Night Airglow on Venus
Planetary and Space Science 85 (2013) 78–88 Contents lists available at ScienceDirect Planetary and Space Science journal homepage: www.elsevier.com/locate/pss Nighttime photochemical model and night airglow on Venus Vladimir A. Krasnopolsky n a Department of Physics, Catholic University of America, Washington, DC 20064, USA b Moscow Institute of Physics and Technology, Dolgoprudnyy 141700 Russia article info abstract Article history: The photochemical model for the Venus nighttime atmosphere and night airglow (Krasnopolsky, 2010, Received 23 December 2012 Icarus 207, 17–27) has been revised to account for the SPICAV detection of the nighttime ozone layer and Received in revised form more detailed spectroscopy and morphology of the OH nightglow. Nighttime chemistry on Venus is 28 April 2013 induced by fluxes of O, N, H, and Cl with mean hemispheric values of 3 Â 1012,1.2Â 109,1010, and Accepted 31 May 2013 − − 1010 cm 2 s 1, respectively. These fluxes are proportional to column abundances of these species in the Available online 18 June 2013 daytime atmosphere above 90 km, and this favors their validity. The model includes 86 reactions of 29 Keywords: species. The calculated abundances of Cl2, ClO, and ClNO3 exceed a ppb level at 80–90 km, and Venus perspectives of their detection are briefly discussed. Properties of the ozone layer in the model agree Photochemistry with those observed by SPICAV. An alternative model without the flux of Cl agrees with the observed O Night airglow 3 peak altitude and density but predicts an increase of ozone to 4 Â 108 cm−3 at 80 km.