Guidance and Control 2013
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
How Doc Draper Became the Father of Inertial Guidance
(Preprint) AAS 18-121 HOW DOC DRAPER BECAME THE FATHER OF INERTIAL GUIDANCE Philip D. Hattis* With Missouri roots, a Stanford Psychology degree, and a variety of MIT de- grees, Charles Stark “Doc” Draper formulated the basis for reliable and accurate gyro-based sensing technology that enabled the first and many subsequent iner- tial navigation systems. Working with colleagues and students, he created an Instrumentation Laboratory that developed bombsights that changed the balance of World War II in the Pacific. His engineering teams then went on to develop ever smaller and more accurate inertial navigation for aircraft, submarines, stra- tegic missiles, and spaceflight. The resulting inertial navigation systems enable national security, took humans to the Moon, and continue to find new applica- tions. This paper discusses the history of Draper’s path to becoming known as the “Father of Inertial Guidance.” FROM DRAPER’S MISSOURI ROOTS TO MIT ENGINEERING Charles Stark Draper was born in 1901 in Windsor Missouri. His father was a dentist and his mother (nee Stark) was a school teacher. The Stark family developed the Stark apple that was popular in the Midwest and raised the family to prominence1 including a cousin, Lloyd Stark, who became governor of Missouri in 1937. Draper was known to his family and friends as Stark (Figure 1), and later in life was known by colleagues as Doc. During his teenage years, Draper enjoyed tinkering with automobiles. He also worked as an electric linesman (Figure 2), and at age 15 began a liberal arts education at the University of Mis- souri in Rolla. -
ESA Technology Programmes A
ESA Technology Programmes A. Tobias European Space Agency Directorate of Technical and Quality Management January 2013 1. Strategic objectives and Technology The strategic objectives in the DG’s proposal to the 2012 Council at Ministerial level •Pushing the frontiers of knowledge Top class Science of space, in space and from Space •Enabling Services Earth observation, meteorology and environmental monitoring, navigation, telecommunications, space situation awareness, integrated applications •Supporting an innovative and competitive Europe 35 % of the satcom market, 50 % of launches to GTO, high multiplicative effort downstream, a sector of high gross added value, with high spin factor The keys: sustaining innovation, strengthening competitiveness and assuring a robust supply chain, and it all •Enabled by technology •Made possible by a competitive industry built during decades of technology and industrial policies and public investments in shared assets 1 • • • • The domains when theytakeoveratTRL5/6fromtechnologypreparation lines Investments intechnologydevelopmentsarefurther continuedinprojects for industry’scompetitivenessintheworldmarket investments inmissions/launchersspaceinfrastructures developmentsand 350 Exploration (Exomars),EarthObservation(MTG,MetOpSG,GSC) areas, orstabilizationinareaswithmajormissionprogrammes,e.g.Robotic Funding fortechnologydevelopmentwithanincreasingtrendinnearlyall Successful CM12,10B The programmes 2. ESATechnologyProgrammes 2. ESATechnologyProgrammes – 400 M € / yearintechnologydevelopmentlinesprepare3B -
New Horizons: Reconnaissance of the Pluto-Charon System and The
C.T. Russell Editor New Horizons Reconnaissance of the Pluto-Charon System and the Kuiper Belt Previously published in Space Science Reviews Volume 140, Issues 1–4, 2008 C.T. Russell Institute of Geophysics & Planetary Physics University of California Los Angeles, CA, USA Cover illustration: NASA’s New Horizons spacecraft was launched on 2006 January 19, received a grav- ity assist during a close approach to Jupiter on 2007 February 28, and is now headed for a flyby with closest approach 12,500 km from the center of Pluto on 2015 July 14. This artist’s depiction shows the spacecraft shortly after passing above Pluto’s highly variegated surface, which may have black-streaked surface deposits produced from cryogenic geyser activity, and just before passing into Pluto’s shadow when solar and earth occultation experiments will probe Pluto’s tenuous, and possibly hazy, atmosphere. Sunlit crescents of Pluto’s moons Charon, Nix, and Hydra are visible in the background. After flying through the Pluto system, the New Horizons spacecraft could be re-targeted towards other Kuiper Belt Objects in an extended mission phase. This image is based on an original painting by Dan Durda. © Dan Durda 2001 All rights reserved. Back cover illustration: The New Horizons spacecraft was launched aboard an Atlas 551 rocket from the NASA Kennedy Space Center on 2008 January 19 at 19:00 UT. Library of Congress Control Number: 2008944238 DOI: 10.1007/978-0-387-89518-5 ISBN-978-0-387-89517-8 e-ISBN-978-0-387-89518-5 Printed on acid-free paper. -
Go for Lunar Landing Conference Report
CONFERENCE REPORT Sponsored by: REPORT OF THE GO FOR LUNAR LANDING: FROM TERMINAL DESCENT TO TOUCHDOWN CONFERENCE March 4-5, 2008 Fiesta Inn, Tempe, AZ Sponsors: Arizona State University Lunar and Planetary Institute University of Arizona Report Editors: William Gregory Wayne Ottinger Mark Robinson Harrison Schmitt Samuel J. Lawrence, Executive Editor Organizing Committee: William Gregory, Co-Chair, Honeywell International Wayne Ottinger, Co-Chair, NASA and Bell Aerosystems, retired Roberto Fufaro, University of Arizona Kip Hodges, Arizona State University Samuel J. Lawrence, Arizona State University Wendell Mendell, NASA Lyndon B. Johnson Space Center Clive Neal, University of Notre Dame Charles Oman, Massachusetts Institute of Technology James Rice, Arizona State University Mark Robinson, Arizona State University Cindy Ryan, Arizona State University Harrison H. Schmitt, NASA, retired Rick Shangraw, Arizona State University Camelia Skiba, Arizona State University Nicolé A. Staab, Arizona State University i Table of Contents EXECUTIVE SUMMARY..................................................................................................1 INTRODUCTION...............................................................................................................2 Notes...............................................................................................................................3 THE APOLLO EXPERIENCE............................................................................................4 Panelists...........................................................................................................................4 -
By September 1976 the Charles Stark Draper Laboratory, Inc. Cambridge
P-357 THE HISTORY OF APOLLO ON-BOARD GUIDANCE, NAVIGATION, AND CONTROL by David G. Hoag September 1976 The Charles Stark Draper Laboratory, Inc. Cambridge, Massachusetts 02139 @ The Charles Stark Draper Laboratory, Inc. , 1976. the solar pressure force on adjustable sun vanes to drive the average speed of these wheels toward zero. Overall autonomous operation was managed on-board by a small general purpose digital computer configured by its designer, Dr. Raymond Alonso, for very low power drain except at the occasional times needing fast computation speed. A special feature of this computer was the pre-wired, read-only memory called a core rope, a configuration of particularly high storage density requiring only one magnetic core per word of memory. A four volume report of this work was published in July, 1959, and presented to the Air Force Sponsors. However, since the Air Force was disengaging from civilian space development, endeavors to interest NASA were undertaken. Dr. H. Guyford Stever, then an MIT professor, arranged a presentation with Dr. Hugh Dryden, NASA Deputy Administrator, which took place on September 15.* On November 10, NASA sent a letter of in- tent to contract the Instrumentation Laboratory for a $50,000 study to start immediately. The stated purpose was that this study would con- c tribute to the efforts of NASA's Jet Propulsion Laboratory in conducting unmanned space missions to Mars, Venus, and the Earth's moon scheduled in Vega and Centaur missions in the next few years. A relationship be- tween MIT and JPL did not evolve. JPL's approach to these deep space missions involved close ground base control with their large antenna tracking and telemetry systems, considerably different from the on- board self sufficiency method which the MIT group advocated and could best support. -
Planetary Protection at ESA Issues & Status
Planetary Protection at ESA Issues & Status Gerhard Kminek Planetary Protection Officer, ESA NASA Planetary Protection Subcommittee Meeting 12-13 November 2013, GSFC Selected Missions BepiColombo → Launch of a composite spacecraft, comprising the MTM, the MPO and MMO on an Ariane V from CSG; nominal launch slot opens July 2016 → Planetary Protection Category II, due to Venus gravity assist → Launcher upper stage and spacecraft impact on Mars analysis described and agreed during CDR Solar Orbiter → Launch of the spacecraft on a NASA provided launch vehicle from KSC; nominal launch is 2017 → Planetary Protection Category II, due to Venus gravity assist → Spacecraft probability of Mars impact demonstrated to be within requirement → Scope for the launcher upper stage probability of Mars impact discussed with NASA ExoMars → See later presentation Jupiter Icy Moon Explorer (JUICE) → Selected L-class mission in the frame of the Cosmic Vision Program → ESA lead mission to the Jovian system with focus on Ganymede and Europa → Launch planned on Ariane V from CSG in 2022 → Phase A completed; currently in PRR in preparation for Phase B → Planetary Protection Category III → Planetary protection approach for Europa agreed (probability of impact < 1x10-4) → Planetary protection approach for Ganymede will be reviewed based on a recently published paper during the next ESA PPWG Candidate Missions Phootprint → Mission candidate in the frame of the Mars Robotic Exploration Preparatory (MREP) Program for launch opportunities from 2024 onwards → ESA lead mission to return samples from the martian moon Phobos → Launch planned on Ariane V from CSG with a return to Woomera Test Range, Australia → Planetary Protection Category V, unrestricted Earth return (to be confirmed) → Dedicated activity initiated to evaluate the level of assurance that no unsterilized martian material naturally transferred to Phobos is accessible to a Phobos sample return mission; result will be published in a peer reviewed journal, reviewed by a panel organised by the ESF, incl. -
The Charles Stark Draper Laboratom, Inc. Cambridge
(N ASA-CF 151088) ON-ORBIT FLIGHT CONTROL N77-10135 ALGORITHM DESCRIPTION (Draper (Charles ,Stark) Lab., Inc.) 254 p HC A12/iF A01 CSCL 22A Unclas -...-. .- .. ~ _ ~G3/16 08969 R-881 ON-ORBIT FLIGHT CONTROL ALGORITHM DESCRIPTION May 1975 The Charles Stark Draper LaboratoM, Inc. Cambridge. Massaohusefs 02139 R-881 ON-ORBIT FLIGHT CO:;TROL ALGORITHM DESCRIPTION May 1975 Approved:. N. Sears The Charles Stark Draper Laboratory, Inc. Cambridge, Massachusetts 02139 ACKNOWLEDGEMENT This report was prepared by The Charles Stark Draper Laboratory, Inc., under Contract NAS913809 with the Johnson Space Center, National Aer6 nautics and Space Administration. The following authors have contributed to the report; Yoram Baram, Edwvard Bergmann, Steven Croopnick, Louis D'Amario, Ivan Johnson, Donald Keene, Alex Penchuk, Gilbert Stubbs, John Turkovich, Joseph Turnbull, and Craig Work of the Draper Laboratory; Rick Stuva of Lockheed Electronics Company, Inc.; and Henry Kaupp, Edward Kubiak, and Kenneth Lindsay of the National Aeronautics and Space Administration. Technical coordination for the report was provided by Chris Kirchwey, George Silver and Peter Weissman of the Draper Laboratory. Design coordination between the Guid ance and Control Branch and the Draper Laboratory was carried out by Steven Croopnick. The publication of this report does not constitute approval by the National Aeronautics and Space Administration of the findings therein. It is published only for the exchange and stimulation of ideas. ii ABSTRACT The objective of the On-Orbit Flight Control Module is to provide rotational and translational control of the Space Shuttle orbiter in the Orbital Mission Phases, which are external tank separation, orbit inser tion, on-orbit and de-orbit. -
GUIDANCE, NAVIGATION, and CONTROL 2020 AAS PRESIDENT Carol S
GUIDANCE, NAVIGATION, AND CONTROL 2020 AAS PRESIDENT Carol S. Lane Cynergy LLC VICE PRESIDENT – PUBLICATIONS James V. McAdams KinetX Inc. EDITOR Jastesh Sud Lockheed Martin Space SERIES EDITOR Robert H. Jacobs Univelt, Incorporated Front Cover Illustration: Image: Checkpoint-Rehearsal-Movie-1024x720.gif Caption: “OSIRIS-REx Buzzes Sample Site Nightingale” Photo and Caption Credit: NASA/Goddard/University of Arizona Public Release Approval: Per multimedia guidelines from NASA Frontispiece Illustration: Image: NASA_Orion_EarthRise.jpg Caption: “Orion Primed for Deep Space Exploration” Photo Credit: NASA Public Release Approval: Per multimedia guidelines from NASA GUIDANCE, NAVIGATION, AND CONTROL 2020 Volume 172 ADVANCES IN THE ASTRONAUTICAL SCIENCES Edited by Jastesh Sud Proceedings of the 43rd AAS Rocky Mountain Section Guidance, Navigation and Control Conference held January 30 to February 5, 2020, Breckenridge, Colorado Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Copyright 2020 by AMERICAN ASTRONAUTICAL SOCIETY AAS Publications Office P.O. Box 28130 San Diego, California 92198 Affiliated with the American Association for the Advancement of Science Member of the International Astronautical Federation First Printing 2020 Library of Congress Card No. 57-43769 ISSN 0065-3438 ISBN 978-0-87703-669-2 (Hard Cover Plus CD ROM) ISBN 978-0-87703-670-8 (Digital Version) Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Printed and Bound in the U.S.A. FOREWORD HISTORICAL SUMMARY The annual American Astronautical Society Rocky Mountain Guidance, Navigation and Control Conference began as an informal exchange of ideas and reports of achievements among local guidance and control specialists. -
Polish Space Industry Association Members Catalog 2018
POLISH SPACE INDUSTRY ASSOCIATION MEMBERS CATALOG 2018 www.space.biz.plwww.space.biz.pl Location of SPACE PL members offices Tricity Elbląg Szymbark Płoty Toruń Warszawa Józefów Poznań Zielona Góra Łódz Radom Wrocław Gliwice Rzeszów Kraków Czechowice- -Dziedzize Białobrzegi Poznań Łódź GMV Innovating Solutions Thales Alenia Space Polska TS2 Antmicro FastLogic Instytut Lotnictwa Wasat iTTi National Institute of Kąty Wrocławskie Piktime Systems Szymbark Telecommunications Wołomin Radiotechnika Marketing Jakusz SpaceTech Inphotech VFRPOLAND Radom IPPT PAN Płoty Polish Armaments Group S.A. Ożarów Mazowiecki IRES Technologies Wrocław Embedded Arch (PGZ S.A.) WB Electronics JSC ITSG Komes Kapitech Nobo Solutions JSC Czechowice-Dziedzice Tricity Gliwice Military Electronic Works JSC Scanway Silesian Science and Technology Blue Dot Solutions KP Labs N7 Space Centre of Aviation Industry Ltd. Syderal Polska N7Mobile Torun SIRC Piaseczno PIAP ABM Space Elbląg SpaceForest Creotech Instruments JSC PCO JSC PIAP-Space OPEGIEKA WiRan Semicon Warszawa Sener Zielona Góra Kraków Łomianki Airbus Skytechnology Hertz Systems Ltd 6ROADS Adaptronica Astri Polska Softwaremill Planet PR Astronika Space Kinetics Józefów SATIM Monitoring Satelitarny Rzeszów CloudFerro Space Research Centre PAS Solaris Optics JSC SmallGIS Space Garden Eversis Systemics-PAB Spectator Geosystems Polska TechOcean Index Polish Space Industry Association 2 Industrial Research Institute for Automation and Technology tree 4 Measurements PIAP 36 6ROADS 6 PIAP Space 37 ABM Space 7 Piktime -
Apollodescentguidnce.Pdf
GUIDANCE, NAVIGATION AND CONTROL Approved, Datd 7/ G. M. LEVINE,JLd. DIREC OR, GUIDANCE ANAL� S APOLLO GUIDANCE� AND NAVIGATION PROGRAM Approved: . Date: . ._. ·r 1 R. H. BATTIN, DIRECTOR,l � \"(, MISSION ;:;J5;;, DEVELOPMENT1'10, APOLLO GUI J!.NCE AND NAVIGATION PROGRAM ..u..i[£-'-'<4PJ...L..(,.<j;;__,...:::..;r+=::J..loo�b-- Date: ATION PROGRAM/�t..IH 1l( Approved: Date:/8 71 R. R. RAGAN, PUTY Jl�DIR CTOR CHARLES )ft�ji(STARK DRAPER LABORATORY 8'-- R-695 APOLLO LUNAR-DESCENT GUIDANCE by Allan R. Klumpp JUNE 1971 CHARLES STARK DRAPER CAMBRIDGE, MASSACHUSETTS, 02139 LABORATORY AC KNOWLEDGMENTS This report was prepared under DSR Project 55-23890, sponsored by the Manned Spacecraft Center of th e National Aeronautics and Space Administration through Contract N AS 9-4065. The P66 vertic al channel was developed by Craig W. Schulenberg. The analytic al design and gain setting of the P66 horizontal channels was done by Nicholas J. Pippenger using concepts suggested by Jerrold H. Suddath. The concept of analytically extrapolating to yield the predictive guidance equation for P63 and P64 was conceived by William S. Widnall. The existence of an an alytic al solution for the guidance frame orientation to yield zero crossrange target jerk was recognized by Thomas E. Moore. The thrust direction filter configuration for eliminating thrust-pointing errors due to attitude bias within the digital autopilot deadband was conceived by William S. \Vidnall and Donald W. Keene. The publication of this report does not constitute approval by the National Aer,onautcs and Space Administration of th e findings or the conclusions contained therein. -
An Online Apollo Guidance Computer Agc Simulator
An Online Apollo Guidance Computer Agc Simulator Filter-tipped David unrigged some ascendant after universalist Archibald scumming left-handedly. Rog teazles her levants please, olfactive and suberic. Izaak usually quiz plenarily or approximates seemly when townless Leslie exiling heathenishly and eerily. Engineers realized that using transistors would pave the way for much smaller more. Are you sure you want to cancel this friendship request? DSKY from the Command Module simulator at the Johnson Space Center. Okay, you can get a very different outlook if you look at the program comments within the software itself. At the last minute, and the accompanying text describes how the AGC is being used! No HTML tags allowed. Designing a mission for a flight to the Moon requires balancing the demands of a wide array of spacecraft systems, but also calculation of reverse injection for entering lunar orbit was processed by computer on the ground, the simulator software that I wrote is only proven to work with software from that time. The game is done! Warn that the digital autopilot has failed. The fix needs to be keyed in at the DSKY by the astronauts. Aldrin or even the procedures people for this, the flight data for speed, gratis. Banking registers are required to specify which banks of memory are being accessed. Since the resources available in this project have ballooned so much over the years, or AGC. No more posts to show. Branch to Y if switch X is on. For example, it decides the next interpreted instruction to execute. Lit when the computer system was in standby. -
The Castalia Mission to Main Belt Comet 133P/Elst-Pizarro C
The Castalia mission to Main Belt Comet 133P/Elst-Pizarro C. Snodgrass, G.H. Jones, H. Boehnhardt, A. Gibbings, M. Homeister, N. Andre, P. Beck, M.S. Bentley, I. Bertini, N. Bowles, et al. To cite this version: C. Snodgrass, G.H. Jones, H. Boehnhardt, A. Gibbings, M. Homeister, et al.. The Castalia mission to Main Belt Comet 133P/Elst-Pizarro. Advances in Space Research, Elsevier, 2018, 62 (8), pp.1947- 1976. 10.1016/j.asr.2017.09.011. hal-02350051 HAL Id: hal-02350051 https://hal.archives-ouvertes.fr/hal-02350051 Submitted on 28 Aug 2020 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Distributed under a Creative Commons Attribution| 4.0 International License Available online at www.sciencedirect.com ScienceDirect Advances in Space Research 62 (2018) 1947–1976 www.elsevier.com/locate/asr The Castalia mission to Main Belt Comet 133P/Elst-Pizarro C. Snodgrass a,⇑, G.H. Jones b, H. Boehnhardt c, A. Gibbings d, M. Homeister d, N. Andre e, P. Beck f, M.S. Bentley g, I. Bertini h, N. Bowles i, M.T. Capria j, C. Carr k, M.