A Review of Spacecraft AI Control Systems
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Venus Aerobot Multisonde Mission
w AIAA Balloon Technology Conference 1999 Venus Aerobot Multisonde Mission By: James A. Cutts ('), Viktor Kerzhanovich o_ j. (Bob) Balaram o), Bruce Campbell (2), Robert Gershman o), Ronald Greeley o), Jeffery L. Hall ('), Jonathan Cameron o), Kenneth Klaasen v) and David M. Hansen o) ABSTRACT requires an orbital relay system that significantly Robotic exploration of Venus presents many increases the overall mission cost. The Venus challenges because of the thick atmosphere and Aerobot Multisonde (VAMuS) Mission concept the high surface temperatures. The Venus (Fig 1 (b) provides many of the scientific Aerobot Multisonde mission concept addresses capabilities of the VGA, with existing these challenges by using a robotic balloon or technology and without requiring an orbital aerobot to deploy a number of short lifetime relay. It uses autonomous floating stations probes or sondes to acquire images of the (aerobots) to deploy multiple dropsondes capable surface. A Venus aerobot is not only a good of operating for less than an hour in the hot lower platform for precision deployment of sondes but atmosphere of Venus. The dropsondes, hereafter is very effective at recovering high rate data. This described simply as sondes, acquire high paper describes the Venus Aerobot Multisonde resolution observations of the Venus surface concept and discusses a proposal to NASA's including imaging from a sufficiently close range Discovery program using the concept for a that atmospheric obscuration is not a major Venus Exploration of Volcanoes and concern and communicate these data to the Atmosphere (VEVA). The status of the balloon floating stations from where they are relayed to deployment and inflation, balloon envelope, Earth. -
Titan and Enceladus $1 B Mission
JPL D-37401 B January 30, 2007 Titan and Enceladus $1B Mission Feasibility Study Report Prepared for NASA’s Planetary Science Division Prepared By: Kim Reh Contributing Authors: John Elliott Tom Spilker Ed Jorgensen John Spencer (Southwest Research Institute) Ralph Lorenz (The Johns Hopkins University, Applied Physics Laboratory) KSC GSFC ARC Approved By: _________________________________ Kim Reh Dr. Ralph Lorenz Jet Propulsion Laboratory The Johns Hopkins University, Applied Study Manager Physics Laboratory Titan Science Lead _________________________________ Dr. John Spencer Southwest Research Institute Enceladus Science Lead Pre-decisional — For Planning and Discussion Purposes Only Titan and Enceladus Feasibility Study Report Table of Contents JPL D-37401 B The following members of an Expert Advisory and Review Board contributed to ensuring the consistency and quality of the study results through a comprehensive review and advisory process and concur with the results herein. Name Title/Organization Concurrence Chief Engineer/JPL Planetary Flight Projects Gentry Lee Office Duncan MacPherson JPL Review Fellow Glen Fountain NH Project Manager/JHU-APL John Niehoff Sr. Research Engineer/SAIC Bob Pappalardo Planetary Scientist/JPL Torrence Johnson Chief Scientist/JPL i Pre-decisional — For Planning and Discussion Purposes Only Titan and Enceladus Feasibility Study Report Table of Contents JPL D-37401 B This page intentionally left blank ii Pre-decisional — For Planning and Discussion Purposes Only Titan and Enceladus Feasibility Study Report Table of Contents JPL D-37401 B Table of Contents 1. EXECUTIVE SUMMARY.................................................................................................. 1-1 1.1 Study Objectives and Guidelines............................................................................ 1-1 1.2 Relation to Cassini-Huygens, New Horizons and Juno.......................................... 1-1 1.3 Technical Approach............................................................................................... -
Visionary Counting on Unmanned Vehicles
Visionary Counting on Unmanned Vehicles By Rich Tuttle Bill Stone, the founder of Stone Aerospace, has a vision—several visions, in fact—and unmanned vehicles play a part in a number of them. His Austin, Texas-based company developed and built the DEPTHX robot that last May conducted the first comprehensive exploration of the world’s deepest sink hole, El Zacaton in Mexico. It brought back enough data to keep scientists enthralled for some time. An unmanned system based on DEPTHX (DEep Phreatic—meaning underwater cave—THermal eXplorer) will be tested in Antarctica beginning next year to help determine the suitability of such a device to meet, in about 20 years, what’s been called the ultimate robotic challenge: exploring the ice- covered ocean of Europa, a moon of Jupiter. Scientists believe there’s a high probability of detecting the first life off Earth in that remote and ancient sea. That's one vision. The challenges would fill a book: melting through many kilometers of ice just to get to the ocean, for instance. That will be addressed in the Antarctica experiments. But DEPTHX does seem to have demonstrated the possibility of clearing two other key hurdles—surviving in a three-dimensional, unexplored environment without external navigation aids; and carrying out science experiments autonomously. DEPTHX's abilities are two generations beyond those of the Spirit and Opportunity rovers on Mars right now, Stone says in an interview. Every move of the Mars vehicles is based on a carefully prepared script. But, Stone says, “in the case of Europa, it can’t be that way.” The computer brain of a Europa probe would have to be wired to achieve “global” objectives, he says. -
Demonstrating Real-World Cooperative Systems Using Aerobots
In Proceedings of the 9th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2006' ESTEC, Noordwijk, The Netherlands, November 28-30, 2006 DEMONSTRATING REAL-WORLD COOPERATIVE SYSTEMS USING AEROBOTS Ehsan Honary1, Frank McQuade1, Roger Ward1, Ian Woodrow2, Andy Shaw3, Dave Barnes3, Matthew Fyfe4 1SciSys [email protected], [email protected], [email protected] Clothier Road, Bristol BS4 5SS, UK TEL: +44 (117) 9717251, FAX: +44 (117) 9721846 2SEA [email protected] Systems Engineering & Assessment Ltd, Beckington Castle, Castle Corner, Beckington, Frome BA11 6TB, UK, TEL: +44 (1373) 852120, FAX: +44 (1373) 831133 3University of Wales Aberystwyth Andy Shaw: [email protected], Dave Barnes: [email protected] Computer Science Department, Penglais, Aberystwyth, Ceredigion, SY23 3DB, Wales, UK TEL: +44 (1970) 621561, FAX: +44 (1970) 622455 4SCS [email protected] Systems Consultants Services Limited, Henley-on-Thames, Oxfordshire, England, RG9 2JN TEL: +44 (1491) 412102, FAX: +44 (1491) 412082 ABSTRACT Use of multiple autonomous robots for practical applications has become more important over the years [1][2][3][4]. The potential for applications of collective robotics is high, in particular in the aerospace environment. SciSys has been involved in the development of Planetary Aerobots funded by ESA for use on Mars and has developed image-based localisation technology as part of the activity. It is however possible to use the Aerobots in a different environment to investigate issues in regard with robotics behaviour such as data handling, communications, limited processing power, limited sensors, GNC, etc. This paper summarises the activity where Aerobot platform was used to investigate the use of multiple autonomous Unmanned Underwater Vehicles (UUVs), basically simulating their movement and behaviour. -
Design and Deployment of a 3D Autonomous Subterranean Submarine Exploration Vehicle
DESIGN AND DEPLOYMENT OF A 3D AUTONOMOUS SUBTERRANEAN SUBMARINE EXPLORATION VEHICLE William C. Stone, Stone Aerospace / PSC, Inc. 3511 Caldwell Lane, Del Valle, TX 78617, Ph: (512) 247-6385, [email protected] ABSTRACT likely include the following components: The NASA Deep Phreatic Thermal Explorer • the parent spacecraft, which will remain in orbit (DEPTHX) project is developing a fully autonomous either about Jupiter or about Europa and which will underwater vehicle intended as a prototype of primarily serve as a data relay back to Earth from the the Europa lander third stage that will search for Lander. microbial life beneath the ice cap of that Jovian • the Lander, which will be a 3-stage device: moon. DEPTHX has two principal objectives: First, to develop and test in an appropriate environment Stage 1: the physical landing system that will contain the ability for an un-tethered robot to explore into propulsion systems, power, and data relay systems to unknown 3D territory, to make a map of what it sees, communicate with the orbiter, and which will control and to use that map to return home; and second, to and carry out the descent and automated landing on demonstrate that science autonomy behaviors can the moon. identify likely zones for the existence of microbial life, to command an autonomous maneuvering Stage 2: the “cryobot” second stage, which will melt platform to move to those locations, conduct localized a hole through up to ten kilometers of ice cap before searches, and to autonomously collect microbial reaching the sub-surface liquid ocean. Although the life in an aqueous environment. -
Energy Efficient Trajectory Generation for a State-Space Based JPL Aerobot
The 2010 IEEE/RSJ International Conference on Intelligent Robots and Systems October 18-22, 2010, Taipei, Taiwan Energy Efficient Trajectory Generation for a State-Space Based JPL Aerobot Weizhong Zhang, Tamer Inanc and Alberto Elfes Abstract— The 40th anniversary of Apollo 11 project with For aerial robotic planetary exploration, some aerial vehi- man landing on the moon reminds the world again by what cles such as airplanes, gliders, helicopters, balloons [4] and science and engineering can do if the man is determined airships [5][6][7][8] have been considered. Airplanes and to do. However, a huge step can only be achieved step by step which may be relatively small at the beginning. Robotic helicopters require significant energy to just stay airborne, exploration can provide necessary information needed to do the flight time of gliders depend mainly on wind, while balloons further step safely, with less cost, more conveniently. Trajectory have limited navigation capabilities. Lighter-Than-Air (LTA) generation for a robotic vehicle is an essential part of the vehicles combine long term mission capability and low total mission planning. To save energy by exploiting possible energy requirement of balloons with the maneuverability of resources such as wind will assist a robotic explorer extend its life span and perform tasks more reliably. In this paper, airplanes. LTA systems, a.k.a. Aerobots or Robotic Airships, we propose to utilize Nonlinear Trajectory Generation (NTG) bring a new opportunity for robotic exploration of planets methodology to generate energy efficient trajectores for the JPL and their moons which have atmosphere. Aerobots can pro- Aerobot by exploiting wind. -
Mabvap: One Step Closer to an Aerobot Mission to Mars
Fifth International Conference on Mars 6119.pdf MABVAP: ONE STEP CLOSER TO AN AEROBOT MISSION TO MARS V.V.Kerzhanovich1, J.A.Cutts1, A.D.Bachelder1, J.M.Cameron1, J.L.Hall1, J.D.Patzold1, M.B.Quadrelli1, A.H.Yavrouian1, J.A.Cantrell2, T. T. Lachenmeier3, M.G.Smith4, 1 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA; 2 Space Dynamics Laboratory, Utah State University, Logan, UT; 3 GSSL, Inc., Hillsboro, OR; 4 Raven Industries, Sulphur Springs, TX Lighter-than-air planetary missions continued attract MABTEX would employ a ~10-m spherical super- growing interest in Mars exploration due to unique pressure balloon with 2.5-3 kg payload providing a combination of proximity to the surface and mobility lifetime in excess of 1 week and possibly much that far surpasses capability of surface vehicles. longer. Recent progress in microminiaturization - Following the experience with the Sojourner rover Sojourner(10 kg) and Muses-C(1.2 kg) rovers, DS-2 and subsequent development of powerful rovers for Mars Microprobes(3.5 kg) - proves that this payload Mars 2003 and 2005 missions it became clear that can serve not only as a technology demonstration but on Mars surface rover mobility is quite restricted. alos can provide a significant opportunity for new Realistic travel distances may be limited to tens of types of scientific measurements. High spatial reso- kilometers per year on relatively obstacle-free plains lution measurements of the remanent magnetic field and a few kilometers or less on the more rugged ter- on Mars, high-resolution imaging and sub-surface rains. -
Development of Small, Mobile, Special-Purpose
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CONTRACT NO. NAS 7-918 TECHNICAL SUPPORT PACKAGE On DEVELOPMENT OF SMALL, MOBILE, SPECIAL-PURPOSE . ROBOTS I for March 98 NASA TECH BRIEF Vol. 22, No. 2, Item #109 from JPL NEW TECHNOLOGY REPORT NPO-20267 Inventor(s): NOTICE Sarita Thakoor Neither the United States Government, nor NASA, nor any person acting on behalf of NASA: a. Makes any warranty or representation, express or implied, with respect of the accuracy, completeness, or usefulness of the information contained in this document, or that the use of any information, apparatus, method, or process disclosed in this document may not infringe privately owned rights; or b. Assumes any liabilities with respect to the use of, or for damages resulting from the use of, any information, apparatus, method or process disclosed in this document. TSP assembled by: JPL Technology Reporting Office pp. i, 1-15 JET PRO PULSION LABORATORY CA LIFO RN IA IN ST IT UTEOF TECHNOLOGY PA SAD EN A, CALIFORNIA March 98 Development of Small, Mobile, Special-Purpose Robots A report presents a scenario for the pro- communicate with fewer larger, more- various robotic tasks. A list of tentative posed development of insectlike robots complex robots, and so forth up a hierar- development goals is presented; the final that would be equipped with microsensors chy to a central robot or instrumentation goal in this list is the demonstration of an and/or micromanipulators, and would be system. The report discusses the historical insectlike exploratory robot in the year designed, variously, to crawl, burrow, background of the concept, presents an 2001 and beyond. -
Mission and System Design of a Venus Entry Probe And
SSC05-V-4 MISSION AND SYSTEM DESIGN OF A VENUS ENTRY PROBE AND AEROBOT Andy Phipps, Adrian Woodroffe, Dave Gibbon, Peter Alcindor, Mukesh Joshi Alex da Silva Curiel, Dr Jeff Ward, Professor Sir Martin Sweeting (SSTL) John Underwood, Dr. Steve Lingard (Vorticity Ltd) Dr Marcel van den Berg, Dr Peter Falkner (European Space Agency) Surrey Satellite Technology Limited University of Surrey, Guildford, Surrey. GU2 7XH, UK Tel: (44) 1483 689278 Fax: (44) 1483 689503 [email protected] Abstract The Venus Entry Probe study is one of ESA's technology reference studies. It aims to identify; the technologies required to develop a low-cost, science-driven mission for in-situ exploration of the atmosphere of Venus, and the philosophy that can be adopted. The mission includes a science gathering spacecraft in an elliptical polar Venus orbit, a relay satellite in highly elliptical Venus orbit, and an atmospheric entry probe delivering a long duration aerobot which will drop several microprobes during its operational phase. The atmospheric entry sequence is initiated at 120 km altitude and an entry velocity of 9.8 kms-1. Once the velocity has reduced to 15 ms-1 the aerobot is deployed. This consists of a gondola and balloon and has a floating mass of 32 kg (which includes 8 kg of science instruments and microprobes). To avoid Venus’ crushing surface pressure and high temperature an equilibrium float altitude of around 55 km has been baselined. The aerobot will circumnavigate Venus several times over a 22-day period analysing the Venusian middle cloud layer. Science data will be returned at 2.5 kbps over the mission duration. -
Autonomous Planning and Execution for a Future Titan Aerobot∗
Autonomous Planning and Execution for a Future Titan Aerobot∗ Daniel Gaines, Tara Estlin, Steve Schaffer, Caroline Chouinard and Alberto Elfes Jet Propulsion Laboratory California Institute of Technology 4800 Oak Grove Drive Pasadena, California 91109 firstname.lastname @jpl.nasa.gov { } Abstract We are developing onboard planning and execution technologies to provide robust and opportunistic mis- sion operations for a future Titan aerobot. Aerobot have the potential for collecting a vast amount of high pri- ority science data. However, to be effective, an aer- obot must address several challenges including com- munication constraints, extended periods without con- tact with Earth, uncertain and changing environmental conditions, maneuvarability constraints and potentially short-lived science opportunities. We are developing the AerOASIS system to develop and test technology to support autonomous science operations for a future Ti- tan Aerobot. The planning and execution component of AerOASIS is able to generate mission operations plans that achieve science and engineering objectives while respecting mission and resource constraints as well as adapting the plan to respond to new science opportuni- ties. Our technology leverages prior work on the OA- SIS system for autonomous rover exploration. In this paper we describe how the OASIS planning component was adapted to address the unique challenges of a Titan Aerobot and we describe a field demonstration of the system with the JPL prototype aerobot. Dune Field Possible Cryovolcano (Huygens) (Cassini VIMS) Introduction NASAs 2008 Solar System Exploration Roadmap (NASA 2008) highlights the importance of aerial probes as a strate- gic new technology for Solar System exploration, and out- lines missions to Venus and Titan that would use airborne vehicles, such as balloons and airships (blimps). -
Inventor Preps Robot to Cut Through Ice on Europa 22 April 2012, by Nancy Owano
Inventor preps robot to cut through ice on Europa 22 April 2012, by Nancy Owano resolve obstacles in the way of studying what may lie beneath Europa's ice. A report in Wired says those obstacles include (1) solar power being unable to work below the surface (2) batteries not lasting long enough (3) too large a footprint of a device and (4) international treaty restrictions that would forbid testing of a nuclear robot. Stone has a 2013-2014 dress rehearsal planned. He intends to test a working cryobot at Alaska's Matanuska Glacier in June next year, where it will attempt to cut through ten to fifty meters of ice. Afterward the cryobot will try to get through 200 meters in Greenland, in fall 2014. Last year, Stone announced that NASA awarded Stone Aerospace four-year, $4M funding to Credit: Stone Aerospace continue development of the Valkyrie project, to design and field-test an autonomous ice penetrating cryobot. Stone, who has a doctorate in structural engineering, is no stranger to such (Phys.org) -- Robots are being developed all the ambitious undertakings. time to do what we wish and to go where we can't. This week, inventor Bill Stone told attendees at Generally, Stone is known for his inventions NASA's Astrobiology Science Conference in designed to enable humans to explore remote Atlanta that he intends to get an autonomous robot environments. He formed Texas-based Stone ready to visit the icebound sea of Jupiter's moon Aerospace to commercialize his systems for Europa, cut through the icy crust, and explore the exploration. -
1 WILLIAM C. STONE, Phd, PE CEO, Stone Aerospace / PSC, Inc. 3511
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