GUIDANCE, NAVIGATION, and CONTROL 2020 AAS PRESIDENT Carol S
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50 Satellite Formation-Flying and Rendezvous
Parkinson, et al.: Global Positioning System: Theory and Applications — Chap. 50 — 2017/11/26 — 19:03 — page 1 1 50 Satellite Formation-Flying and Rendezvous Simone D’Amico1) and J. Russell Carpenter2) 50.1 Introduction to Relative Navigation GNSS has come to play an increasingly important role in satellite formation-flying and rendezvous applications. In the last decades, the use of GNSS measurements has provided the primary method for determining the relative position of cooperative satellites in low Earth orbit. More recently, GNSS data have been successfully used to perform formation-flying in highly elliptical orbits with apogees at tens of Earth radii well above the GNSS constellations. Current research aims at dis- tributed precise relative navigation between tens of swarming nano- and micro-satellites based on GNSS. Similar to terrestrial applications, GNSS relative navigation benefits from a high level of common error cancellation. Furthermore, the integer nature of carrier phase ambiguities can be exploited in carrier phase differential GNSS (CDGNSS). Both aspects enable a substantially higher accuracy in the estimation of the relative motion than can be achieved in single-spacecraft navigation. Following historical remarks and an overview of the state-of-the-art, this chapter addresses the technology and main techniques used for spaceborne relative navigation both for real-time and offline applications. Flight results from missions such as the Space Shuttle, PRISMA, TanDEM-X, and MMS are pre- sented to demonstrate the versatility and broad range of applicability of GNSS relative navigation, from precise baseline determination on-ground (mm-level accuracy), to coarse real-time estimation on-board (m- to cm-level accuracy). -
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering Laurel Mossman, Kate Schein, and Amelia Peoples Senior Division Group Documentary Word Count: 499 Our group chose the topic, Donna Shirley and her Mars rover, because of our connections and our interest level in not only science but strong, determined women. One of our group member’s mothers worked for a man under Ms. Shirley when she was developing the Mars rover. This provided us with a connection to Ms. Shirley, which then gave us the amazing opportunity to interview her. In addition, our group is interested in the philosophy of equality and we have continuously created documentaries that revolve around this idea. Every member of our group is a female, so we understand the struggles and discrimination that women face in an everyday setting and wanted to share the story of a female that faced these struggles but overcame them. Thus after conducting a great amount of research, we fell in love with Donna Shirley’s story. Lastly, it was an added benefit that Ms. Shirley is from Oklahoma, making her story important to our state. All of these components made this topic extremely appealing to us. We conducted our research using online articles, Donna Shirley’s autobiography, “Managing Martians”, news coverage from the launch day, and our interview with Donna Shirley. We started our research process by reading Shirley’s autobiography. This gave us insight into her college life, her time working at the Jet Propulsion Laboratory, and what it was like being in charge of such a barrier-breaking mission. -
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. -
Annual Report 2014 OUR VISION
AMOS Centre for Autonomous Marine Operations and Systems Annual Report 2014 Annual Report OUR VISION To establish a world-leading research centre for autonomous marine operations and systems: To nourish a lively scientific heart in which fundamental knowledge is created through multidisciplinary theoretical, numerical, and experimental research within the knowledge fields of hydrodynamics, structural mechanics, guidance, navigation, and control. Cutting-edge inter-disciplinary research will provide the necessary bridge to realise high levels of autonomy for ships and ocean structures, unmanned vehicles, and marine operations and to address the challenges associated with greener and safer maritime transport, monitoring and surveillance of the coast and oceans, offshore renewable energy, and oil and gas exploration and production in deep waters and Arctic waters. Editors: Annika Bremvåg and Thor I. Fossen Copyright AMOS, NTNU, 2014 www.ntnu.edu/amos AMOS • Annual Report 2014 Table of Contents Our Vision ........................................................................................................................................................................ 2 Director’s Report: Licence to Create............................................................................................................................. 4 Organization, Collaborators, and Facts and Figures 2014 ......................................................................................... 6 Presentation of New Affiliated Scientists................................................................................................................... -
Development of the Crew Dragon ECLSS
ICES-2020-333 Development of the Crew Dragon ECLSS Jason Silverman1, Andrew Irby2, and Theodore Agerton3 Space Exploration Technologies, Hawthorne, California, 90250 SpaceX designed the Crew Dragon spacecraft to be the safest ever flown and to restore the ability of the United States to launch astronauts. One of the key systems required for human flight is the Environmental Control and Life Support System (ECLSS), which was designed to work in concert with the spacesuit and spacecraft. The tight coupling of many subsystems combined with an emphasis on simplicity and fault tolerance created unique challenges and opportunities for the design team. During the development of the crew ECLSS, the Dragon 1 cargo spacecraft flew with a simple ECLSS for animals, providing an opportunity for technology development and the early characterization of system-level behavior. As the ECLSS design matured a series of tests were conducted, including with humans in a prototype capsule in November 2016, the Demo-1 test flight to the ISS in March 2019, and human-in-the-loop ground testing in the Demo-2 capsule in January 2020 before the same vehicle performs a crewed test flight. This paper describes the design and operations of the ECLSS, the development process, and the lessons learned. Nomenclature AC = air conditioning AQM = air quality monitor AVV = active vent valve CCiCap = Commercial Crew Integrated Capability CCtCap = Commercial Crew Transportation Capability CFD = computational fluid dynamics conops = concept of operations COPV = composite overwrapped -
Solar Aircraft Design
Cumhuriyet Üniversitesi Fen Fakültesi Cumhuriyet University Faculty of Science Fen Bilimleri Dergisi (CFD), Cilt:36, No: 3 Özel Sayı (2015) Science Journal (CSJ), Vol. 36, No: 3 Special Issue (2015) ISSN: 1300-1949 ISSN: 1300-1949 SOLAR AIRCRAFT DESIGN Sadegh RAHMATI1,*, Amir GHASED2 1,2Department of Mechanical Engineering, Majlesi Branch, Islamic Azad University, Isfahan, Iran Received: 01.02.2015; Accepted: 05.05.2015 ______________________________________________________________________________________________ Abstract. Generally domain Aircraft uses conventional fuel. These fuel having limited life, high cost and pollutant. Also nowadays price of petrol and other fuels are going to be higher, because of scarcity of those fuels. So there is great demand of use of non-exhaustible unlimited source of energy like solar energy. Solar aircraft is one of the ways to utilize solar energy. Solar aircraft uses solar panel to collect the solar radiation for immediate use but it also store the remaining part for the night flight. This paper intended to stimulate research on renewable energy sources for aviation. In future solar powered air planes could be used for different types of aerial momitoring and unmanned flights. This review paper brietly shows history, application and use of solar aircraft. We are focusing on design and fabrication of solar aircraft which is unmanned prototype. Keywords: Solar energy, Reynolds number, Bernoulli’s principle 1. INTRODUCTION Energy comes in different forms. Light is a form of energy. Sun is source of energy called “sunlight”. Sunshine is free and never gets used up Also. There is a lot of it. The sunlight that heats the Earth in an hour has more energy than the people of the world use in a year. -
Galileo FOC-M7 SAT 19-20-21-22
LAUNCH KIT December 2017 VA240 Galileo FOC-M7 SAT 19-20-21-22 VA240 Galileo FOC-M7 SAT 19-20-21-22 ARIANESPACE’S SECOND ARIANE 5 LAUNCH FOR THE GALILEO CONSTELLATION AND EUROPE For its 11th launch of the year, and the sixth Ariane 5 liftoff from the Guiana Space Center (CSG) in French Guiana during 2017, Arianespace will orbit four more satellites for the Galileo constellation. This mission is being performed on behalf of the European Commission under a contract with the European Space Agency (ESA). For the second time, an Ariane 5 ES version will be used to orbit satellites in Europe’s own satellite navigation system. At the completion of this flight, designated Flight VA240 in Arianespace’s launcher family numbering system, 22 Galileo spacecraft will have been launched by Arianespace. Arianespace is proud to deploy its entire family of launch vehicles to address Europe’s needs and guarantee its independent access to space. Galileo, an iconic European program Galileo is Europe’s own global navigation satellite system. Under civilian control, Galileo offers guaranteed high-precision positioning around the world. Its initial services began in December CONTENTS 2016, allowing users equipped with Galileo-enabled devices to combine Galileo and GPS data for better positioning accuracy. The complete Galileo constellation will comprise a total of 24 operational satellites (along with > THE LAUNCH spares); 18 of these satellites already have been orbited by Arianespace. ESA transferred formal responsibility for oversight of Galileo in-orbit operations to the GSA VA240 mission (European GNSS Agency) in July 2017. Page 3 Therefore, as of this launch, the GSA will be in charge of the operation of the Galileo satellite Galileo FOC-M7 satellites navigation systems on behalf of the European Union. -
State of the Art of Piloted Electric Airplanes, NASA's Centennial Challenge Data and Fundamental Design Implications
Dissertations and Theses Fall 2011 State of the Art of Piloted Electric Airplanes, NASA's Centennial Challenge Data and Fundamental Design Implications Lori Anne Costello Embry-Riddle Aeronautical University - Daytona Beach Follow this and additional works at: https://commons.erau.edu/edt Part of the Aerospace Engineering Commons Scholarly Commons Citation Costello, Lori Anne, "State of the Art of Piloted Electric Airplanes, NASA's Centennial Challenge Data and Fundamental Design Implications" (2011). Dissertations and Theses. 37. https://commons.erau.edu/edt/37 This Thesis - Open Access is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Dissertations and Theses by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. STATE OF THE ART OF PILOTED ELECTRIC AIRPLANES, NASA’S CENTENNIAL CHALLENGE DATA AND FUNDAMENTAL DESIGN IMPLICATIONS by Lori Anne Costello A Thesis Submitted to the Graduate Studies Office in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aerospace Engineering Embry-Riddle Aeronautical University Daytona Beach, Florida Fall 2011 1 Copyright by Lori Anne Costello 2011 All Rights Reserved 2 ACKNOWLEDGEMENTS This thesis is the culmination of two years of work on the Green Flight Challenge Eco-Eagle. The Eco- Eagle and this thesis would not have been possible without countless help and inspiration from friends and family. I would like to thank Dr. Anderson for giving me the opportunity to participate in Embry-Riddle’s Green Flight Challenge Team and for supporting me and the Eco-Eagle project. Without his guidance I would not have this paper and understood as much as I now do about electric airplanes. -
Developing Technologies for Biological Experiments in Deep Space
Developing technologies for biological experiments in deep space Sergio R. Santa Maria Elizabeth Hawkins Ada Kanapskyte NASA Ames Research Center [email protected] NASA’s life science programs STS-1 (1981) STS-135 (2011) 1973 – 1974 1981 - 2011 2000 – 2006 – Space Shuttle International Skylab Bio CubeSats Program Space Station Microgravity effects - Nausea / vomit - Disorientation & sleep loss - Body fluid redistribution - Muscle & bone loss - Cardiovascular deconditioning - Increase pathogenicity in microbes Interplanetary space radiation What type of radiation are we going to encounter beyond low Earth orbit (LEO)? Galactic Cosmic Rays (GCRs): - Interplanetary, continuous, modulated by the 11-year solar cycle - High-energy protons and highly charged, energetic heavy particles (Fe-56, C-12) - Not effectively shielded; can break up into lighter, more penetrating pieces Challenges: biology effects poorly understood (but most hazardous) Interplanetary space radiation Solar Particle Events (SPEs) - Interplanetary, sporadic, transient (several min to days) - High proton fluxes (low and medium energy) - Largest doses occur during maximum solar activity Challenges: unpredictable; large doses in a short time Space radiation effects Space radiation is the # 1 risk to astronaut health on extended space exploration missions beyond the Earth’s magnetosphere • Immune system suppression, learning and memory impairment have been observed in animal models exposed to mission-relevant doses (Kennedy et al. 2011; Britten et al. 2012) • Low doses of space radiation are causative of an increased incidence and early appearance of cataracts in astronauts (Cuccinota et al. 2001) • Cardiovascular disease mortality rate among Apollo lunar astronauts is 4-5-fold higher than in non-flight and LEO astronauts (Delp et al. -
NASA APPEL 2013 Annual Report
National Aeronautics and Space Administration Annual Report Fiscal Year 2013 Academy of Program/Project & Engineering Leadership (APPEL) www.nasa.gov Table of Contents 3 About the Academy 3 Mission and Goals 4 Leadership Team 5 Executive Summary 7 Core Business 9 Innovations and Cost Management 13 Building Individual Capability Through Training 17 Learning Through Hands-On Experience 22 CKO – Promoting a Learning Organization Through Knowledge Services 26 Learning and Working Through International Collaboration 28 Meeting the Needs of Young Professionals 30 Facilitating Open Communication and Dialogue 32 2014 Outlook 2 About the Academy Before assuming its present structure, the NASA Academy of Program/Project & Engineering Leadership (APPEL) underwent several metamorphoses in response to changing needs at the agency. Beginning with the Program and Project Management Initiative (PPMI) in 1988, which was founded in response to the Challenger disaster, NASA leadership identified a need to develop program and project management excellence in the workforce through training. Ten years later, the agency outgrew the PPMI model as its mission portfolio and workforce evolved. The renamed APPEL grew to place a greater emphasis on curriculum, certification, team performance, and knowledge sharing across NASA. Since then, the Academy’s initiatives have provided support to the agency’s technical workforce through its integrated curriculum, team support services, and knowledge sharing activities. In January 2012, a Congressionally established advisory group called the Aerospace Safety Advisory Panel, recommended that NASA establish a single focal point within the agency to develop the policy and requirements necessary to integrate knowledge capture across programs, projects, and centers. In response, NASA appointed its first-ever agency-wide Chief Knowledge Officer (CKO), building upon of the wealth of knowledge sharing activities already underway across NASA, including APPEL. -
Commercial Orbital Transportation Services
National Aeronautics and Space Administration Commercial Orbital Transportation Services A New Era in Spaceflight NASA/SP-2014-617 Commercial Orbital Transportation Services A New Era in Spaceflight On the cover: Background photo: The terminator—the line separating the sunlit side of Earth from the side in darkness—marks the changeover between day and night on the ground. By establishing government-industry partnerships, the Commercial Orbital Transportation Services (COTS) program marked a change from the traditional way NASA had worked. Inset photos, right: The COTS program supported two U.S. companies in their efforts to design and build transportation systems to carry cargo to low-Earth orbit. (Top photo—Credit: SpaceX) SpaceX launched its Falcon 9 rocket on May 22, 2012, from Cape Canaveral, Florida. (Second photo) Three days later, the company successfully completed the mission that sent its Dragon spacecraft to the Station. (Third photo—Credit: NASA/Bill Ingalls) Orbital Sciences Corp. sent its Antares rocket on its test flight on April 21, 2013, from a new launchpad on Virginia’s eastern shore. Later that year, the second Antares lifted off with Orbital’s cargo capsule, (Fourth photo) the Cygnus, that berthed with the ISS on September 29, 2013. Both companies successfully proved the capability to deliver cargo to the International Space Station by U.S. commercial companies and began a new era of spaceflight. ISS photo, center left: Benefiting from the success of the partnerships is the International Space Station, pictured as seen by the last Space Shuttle crew that visited the orbiting laboratory (July 19, 2011). More photos of the ISS are featured on the first pages of each chapter. -
The Navy Navigation Satellite System (Transit)
ROBERT J. DANCHIK THE NAVY NAVIGATION SATELLITE SYSTEM (TRANSIT) This article provides an update on the status of the Navy Navigation Satellite System (TRANSIT). Some insights are provided on the evolution of the system into its current configuration, as well as a discussion of future plans. BACKGROUND sign goal was never achieved for long in those early In 1958, research scientists at APL solved the orbit days because the satellites had short operational life of the first Russian satellite, Sputnik-I, by analysis of times. The failures largely resulted from inadequate the observed Doppler shift of its transmitted signal. component quality and the large number of wiring in This led immediately to the concept of satellite navi terconnections. However, after OSCAR 2 10 and OS gation and the development of the U.S. Navy Navi CAR 12 were launched in 1966 and 1967, respectively, gation Satellite System (TRANSIT) by APL, under the enough data on the failure mechanisms became avail sponsorship of the Navy's Special Projects Office, to able to APL to achieve the desired advances in reli provide position fixes for the Fleet Ballistic Missile ability. The integrated circuit introduced in OSCAR Weapon System submarines. (The articles in Ref. 1, 10 significantly extended the satellite lifetime by im a previous issue of the fohns Hopkins APL Techni proving component reliability and reducing the num cal Digest devoted to TRANSIT, give the principles ber of interconnections. Subsequently, the last major of operation and early history of the system.) Now, design change made to the solar cell interconnections, 26 years after its conception, the system is mature.