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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. -
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. -
National Academy of Sciences July 1, 1979 Officers
NATIONAL ACADEMY OF SCIENCES JULY 1, 1979 OFFICERS Term expires President-PHILIP HANDLER June 30, 1981 Vice-President-SAUNDERS MAC LANE June 30, 1981 Home Secretary-BRYCE CRAWFORD,JR. June 30, 1983 Foreign Secretary-THOMAS F. MALONE June 30, 1982 Treasurer-E. R. PIORE June 30, 1980 Executive Officer Comptroller Robert M. White David Williams COUNCIL Abelson, Philip H. (1981) Markert,C. L. (1980) Berg, Paul (1982) Nierenberg,William A. (1982) Berliner, Robert W. (1981) Piore, E. R. (1980) Bing, R. H. (1980) Ranney, H. M. (1980) Crawford,Bryce, Jr. (1983) Simon, Herbert A. (1981) Friedman, Herbert (1982) Solow, R. M. (1980) Handler, Philip (1981) Thomas, Lewis (1982) Mac Lane, Saunders (1981) Townes, Charles H. (1981) Malone, Thomas F. (1982) Downloaded by guest on September 30, 2021 SECTIONS The Academyis divided into the followingSections, to which membersare assigned at their own choice: (11) Mathematics (31) Engineering (12) Astronomy (32) Applied Biology (13) Physics (33) Applied Physical and (14) Chemistry Mathematical Sciences (15) Geology (41) Medical Genetics Hema- (16) Geophysics tology, and Oncology (21) Biochemistry (42) Medical Physiology, En- (22) Cellularand Develop- docrinology,and Me- mental Biology tabolism (23) Physiological and Phar- (43) Medical Microbiology macologicalSciences and Immunology (24) Neurobiology (51) Anthropology (25) Botany (52) Psychology (26) Genetics (53) Social and Political Sci- (27) Population Biology, Evo- ences lution, and Ecology (54) Economic Sciences In the alphabetical list of members,the numbersin parentheses, followingyear of election, indicate the respective Class and Section of the member. CLASSES The members of Sections are grouped in the following Classes: I. Physical and Mathematical Sciences (Sections 11, 12, 13, 14, 15, 16). -
E Helsinki Forum and East-West Scientific Exchange
[E HELSINKI FORUM AND EAST-WEST SCIENTIFIC EXCHANGE JOINT HEARING BEFORE THE SUBCOMMITTEE ON SCIENCE, RESEARCH AND TECHNOLOGY OF THE COMMITTEE ON SCIENCE AND TECHNOLOGY AND THE Sul COMMITTEE ON INTERNATIONAL SECURITY AND SCIENTIFIC AFFAIRS OF THE COMMITTEE ON FOREIGN AFFAIRS HOUSE OF REPRESENTATIVES AND THE COMMISSION ON SECURITY AND COOPERATION IN EUROPE NINETY-SIXTH CONGRESS SECOND SESSION JANUARY 31, 1980 [No. 89] (Committee on Science and Technology) ted for the use of the Committee on Science and Technology and the Committee on Foreign Affairs U.S. GOVERNMENT PRINTING OFFICE 421 0 WASHINGTON: 1980 COMMITTEE ON SCIENCE AND TECHNOLOGY DON FUQUA, Florida, Chairman ROBERT A. ROE, New Jersey JOHN W. WYDLER, New York MIKE McCORMACK, Washington LARRY WINN. JR., Kansas GEORGE E. BROWN, JR., California BARRY M. GOLDWATER, JR., California JAMES H. SCHEUER, New York HAMILTON FISH, JS., New York RICHARD L. OTTINGER, New York MANUEL LUJAN, JR., New Mexico TOM HARKIN, Iowa HAROLD C. HOLLENBECK, New Jersey JIM LLOYD, California ROBERT K. DORNAN, California JEROME A. AMBRO, New York ROBERT S. WALKER, Pennsylvania MARILYN LLOYD BOUQUARD, Tennessee EDWIN B. FORSYTHE, NeW Jersey JAMES J. BLANCHARD, Michigan KEN KRAMER, Colorado DOUG WALGREN, Pennsylvania WILLIAM CARNEY, New York RONNIE G. FLIPPO, Alabama ROBERT W. DAVIS, Michigan DAN GLICKMAN, Kansas TOBY ROTH, Wisconsin ALBERT GORE, JR., Tennessee DONALD LAWRENCE RITTER, WES WATKINS, Oklahoma Pennsylvania ROBERT A. YOUNG, Missouri BILL ROYER, California RICHARD C. WHITE, Texas HAROLD L. VOLKMER, Missouri DONALD J. PEASE, Ohio HOWARD WOLPE, Michigan NICHOLAS MAVROULES, Massachusetts BILL NELSON, Florida BERYL ANTHONY, JR., Arkansas STANLEY N. LUNDINE, New York ALLEN E. -
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. -
Supplementary Figure 1: Interconnected Multiplex with Six Nodes in Two Layers (A and D) and Corresponding Aggregated Networks (B and E)
Supplementary Figure 1: Interconnected multiplex with six nodes in two layers (A and D) and corresponding aggregated networks (B and E). The nodes are ranked by their eigenvector centrality in each layer separately, in the aggregated and in the whole interconnected structure (C and F). Case A, B and C. Nodes 1 and 3 have a key role in the multilayer, being bridges between the two layers. In a collaboration network they would represent scientists working on two different research areas who allow information to flow from one subject to the other. While nodes 1 and 3 gain centrality from their connections to \hubs" on different layers, they also gain centrality from their own counterparts in other layers, making them important in the multilayer network. In the aggregated network their versatility disappears, because the information is washed out by projecting on a single layer, where nodes 2 and 6 are still \hubs" but it is not possible to capture the importance of nodes 1 and 3 in bridging different areas. Case D, E and F. This example shows how aggregating the full information on a single network introduces a spurious symmetry between nodes 2, 3, 4 and 6 that is not present in the multilayer, except for 2 and 4. The resulting score in the aggregate is not able to capture the difference between these nodes (corresponding to a degeneration in the eigenspace) while it is evident that, for instance, node 6 is more central than node 3 because of its direct connection to node 1 { the \hub" { in layer 1. -
Oxford University Press Free Sample Chapter Multiplex-Multi-Level
FREE SAMPLE CHAPTER Networks and Complex Systems publications from Oxford University Press 30% online discount Networks Multilayer Networks Introduction to the Second Edition Structure and Function Theory of £49.99 £34.99 £55.00 £38.50 Complex Systems Mark Newman Ginestra Bianconi £49.99 £34.99 Stefan Thurner, Peter Klimek, Rudolf Hanel Generating Random Scale-Free Networks Agent-Based Modeling Networks and Graphs Complex Webs in and Network Dynamics £55.00 £38.50 Nature and Technology £57.50 £40.25 Ton Coolen, Alessia Annibale, £34.49 £24.14 Akira Namatame, Ekaterina Roberts Guido Caldarelli Shu-Heng Chen Order online at www.oup.com and enter the code EXCCS-18 to get a 30% discount Visit us at stand #1 to receive your free hard copy of this chapter and join our mailing list. OUP UNCORRECTED PROOF – FIRST PROOF, 3/8/2018, SPi Preface As the field of complex networks entered its maturity phase, most scientists working in this field thought that the established methodology could deal with all casesof networked systems. However, as is usually the case in the scientific enterprise, some novel observations showed that what we already know is only a limited case, and network theory has still long way to go until we can make any definitive claim. The ever-increasing availability of data in fields ranging from computer science to urban systems, medicine, economics, and finance showed that networks that were usually perceived as distinct and isolated are, in reality, interacting with other networks. While this sounds like a trivial observation, it was shown that interactions of different networks can lead to unexpected behaviors and allow systemic vulnerabilities to emerge. -
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. -
UNITED STATES PATENT OFFICE 2,478,916 REFORMING Process Vladimir Haensel, Clarendon Hills, and Curtis F
Patented Aug. 16, 1949 2.478,916 UNITED STATES PATENT OFFICE 2,478,916 REFORMING PRocess Vladimir Haensel, Clarendon Hills, and Curtis F. Gerald, Riverside, E., assignors to Universa Oil Products Company, Chicago, I., a corporation of Delaware No Drawing. Application December 21, 1946, Serial No. 71,659 13 Claims. (Cl 196-50) 2 This invention relates to a reforming process mally liquid hydrocarbons substantially or con and more particularly to a process for the re pletely into normally gaseous hydrocarbons. forming of a saturated gasoline fraction in the The desired selective cracking generally com presence of a particular catalyst and under se prises the removal of methyl, ethyl and, to a lected conditions of operation. lesser extent, propyl groups, in the form of The saturated gasoline fraction to be treat methane, ethane and propane as will be herein ed in accordance with the present invention after described. However, the removal of these comprise straight run gasolines, natural gaso radicals is controlled so that not more than. One lines, etc. The gasoline fraction may be a full or possibly two of such radicals are removed boiling range gasoline having an initial boiling O from a given molecule. For example, heptane point within the range of about 50 to about may be reduced to hexane, nonane to Octane or 90 F. and an end boiling point within the heptane, etc. On the other hand uncontrolled range of about 375 to about 4.25° F., or it may or non-selective cracking will result in the de be a selected fraction thereof which usually will composition of normally liquid hydrocarbons be a higher boiling fraction, commonly referred into normally gaseous hydrocarbons as, for ex to as naphtha, and generally having an initial ample, by the continued demethylation of nor boiling point of from about 150 to about 250 F. -
Memorial Tributes: Volume 15
THE NATIONAL ACADEMIES PRESS This PDF is available at http://nap.edu/13160 SHARE Memorial Tributes: Volume 15 DETAILS 444 pages | 6 x 9 | HARDBACK ISBN 978-0-309-21306-6 | DOI 10.17226/13160 CONTRIBUTORS GET THIS BOOK National Academy of Engineering FIND RELATED TITLES Visit the National Academies Press at NAP.edu and login or register to get: – Access to free PDF downloads of thousands of scientific reports – 10% off the price of print titles – Email or social media notifications of new titles related to your interests – Special offers and discounts Distribution, posting, or copying of this PDF is strictly prohibited without written permission of the National Academies Press. (Request Permission) Unless otherwise indicated, all materials in this PDF are copyrighted by the National Academy of Sciences. Copyright © National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 15 Memorial Tributes NATIONAL ACADEMY OF ENGINEERING Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 15 Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 15 NATIONAL ACADEMY OF ENGINEERING OF THE UNITED STATES OF AMERICA Memorial Tributes Volume 15 THE NATIONAL ACADEMIES PRESS Washington, D.C. 2011 Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 15 International Standard Book Number-13: 978-0-309-21306-6 International Standard Book Number-10: 0-309-21306-1 Additional copies of this publication are available from: The National Academies Press 500 Fifth Street, N.W. Lockbox 285 Washington, D.C. 20055 800–624–6242 or 202–334–3313 (in the Washington metropolitan area) http://www.nap.edu Copyright 2011 by the National Academy of Sciences. -
Catalysis: Change for the Better
Catalysis: Change for the Better Grade Level petroleum into the high-level fuels that we rely on for nearly all our transportation Elementary through middle school with adult needs. It also produces "aromatic" assistance. petrochemicals, the raw materials used in the manufacture of plastics and fibers. High school This new idea in catalysts, and the ideas Materials that followed, have made our fuel more efficient, environmentally-friendly and easier Ordinary sugar cubes and cheaper to produce. It has also made Matches the plastics industry more environmentally- Ash friendly. Metal plate or can lid In 1998, Vladimir Haensel received the Charles Stark Draper Prize, a $450,000 Discussion award, for his work. This award is the "Nobel Prize" of engineering. it is presented by the Sometimes a chemical reaction won't take National Academy of Engineering, with an place, or will proceed very slowly, unless endowment from the Charles Stark Draper some other substance is added. That other Laboratory. Charles Stark Draper was an substance is called a catalyst, which engineer and "father" of modern inertial hastens the action but is not part of it and guidance systems, used in commercial does not change. Catalysts are widely used aircraft, space vehicles, strategic missiles, in the chemical industry to speed up and submarines. Draper also developed the reactions. An important use of catalysts is in sophisticated navigational system that the making of gasoline from crude oil. landed the Apollo astronauts on the moon and returned them safely to earth. In 1949 at Universal Oil Products (now UOP), chemical engineer Vladimir Haensel developed a revolutionary process called Platforming.