Micro-Satellite Data Handling: a Unified Information Model
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Software Problems of an Experimental Robot
PERIODICA POLITECHHICA SER EL ENG. VOL 46, NO J-J. PP. 151-16112002) SOFTWARE PROBLEMS OF AN EXPERIMENTAL ROBOT CONTROLLER BASED ON QNX REAL-TIME OPERATING SYSTEMS Istvan OLAH and Gdbor TEVESZ Department of Auiomation and Applied Informatics Budapest University of Technology and Economics H-l 111 Budapest, Goldmann Gyorgy tc"r 3. Hungary Phone: (+36-1)463-2870, Fax: (436-1)463-2871 e-mail: [email protected]; [email protected] Received: July 1,2003 Abstract At the Department of Automation and Applied Informatics an experimental robot control system has been developed. The purpose of this research is to study modern robot control algorithms and their realization in a real environment. The project focuses on the problems of multiprocessor systems including the task distribution and communication. Another field of this research is to integrate a six-component forcc-torquc sensor into the robot control system and making use of this information in new robot control algorithms. Another purpose of this study is to examine the software problems of an IBM PC-based multiprocessor system controlling a NOKIA-PUMA 560 humanoid robot arm. The features and system services of the new QNX Neutrino operating system is presented in comparison with the previously used QNX v4. The main areas of the version upgrade will be shown focusing on the interprocess communication questions. The processing components of this multiprocessor robot control system with its external interfaces will be discussed later and some further system level development possibilities will be outlined. This final part of the study gives the summary of the architectural and communication requirements of a hybrid position and force control system in the above environment. -
2015 October
TTSIQ #13 page 1 OCTOBER 2015 www.nasa.gov/press-release/nasa-confirms-evidence-that-liquid-water-flows-on-today-s-mars Flash! Sept. 28, 2015: www.space.com/30674-flowing-water-on-mars-discovery-pictures.html www.space.com/30673-water-flows-on-mars-discovery.html - “boosting odds for life!” These dark, narrow, 100 meter~yards long streaks called “recurring slope lineae” flowing downhill on Mars are inferred to have been formed by contemporary flowing water www.space.com/30683-mars-liquid-water-astronaut-exploration.html INDEX 2 Co-sponsoring Organizations NEWS SECTION pp. 3-56 3-13 Earth Orbit and Mission to Planet Earth 13-14 Space Tourism 15-20 Cislunar Space and the Moon 20-28 Mars 29-33 Asteroids & Comets 34-47 Other Planets & their moons 48-56 Starbound ARTICLES & ESSAY SECTION pp 56-84 56 Replace "Pluto the Dwarf Planet" with "Pluto-Charon Binary Planet" 61 Kepler Shipyards: an Innovative force that could reshape the future 64 Moon Fans + Mars Fans => Collaboration on Joint Project Areas 65 Editor’s List of Needed Science Missions 66 Skyfields 68 Alan Bean: from “Moonwalker” to Artist 69 Economic Assessment and Systems Analysis of an Evolvable Lunar Architecture that Leverages Commercial Space Capabilities and Public-Private-Partnerships 71 An Evolved Commercialized International Space Station 74 Remembrance of Dr. APJ Abdul Kalam 75 The Problem of Rational Investment of Capital in Sustainable Futures on Earth and in Space 75 Recommendations to Overcome Non-Technical Challenges to Cleaning Up Orbital Debris STUDENTS & TEACHERS pp 85-96 Past TTSIQ issues are online at: www.moonsociety.org/international/ttsiq/ and at: www.nss.org/tothestarsOO TTSIQ #13 page 2 OCTOBER 2015 TTSIQ Sponsor Organizations 1. -
The SUNSAT Micro Satellite Program
The SUNSAT Micro Satellite Program: Technical performance and limits of imaging micro satellites Sias Mostert, Thys Cronje and Francois du Plessis Department of Electrical and Electronic Engineering Stellenbosch University. Private Bag X1, MATIELAND, 7602. South Africa. Fax: +27 21 808 4981. Internet: [email protected]. http:\\sunsat.ee.sun.ac.za ABSTRACT - This paper examines the technical performance of the SUNSAT micro satellite bus, which is supporting the high resolution imager (HRI) payload on the micro satellite which is scheduled for launch in December 1998. A number of existing remote sensing satellites are investigated to determine some key parameters by which a micro satellite remote sensing mission should be evaluated. The SUNSAT 1 HRI instrument is then evaluated in this context and future possible missions suggested which is suitable for micro satellite missions. 1. INTRODUCTION SUNSAT, a professional micro satellite developed by a team of graduate students and engineers at Stellenbosch University in South Africa, is scheduled for launch from Vandenberg Airforce Base on a Delta II rocket, currently manifested for December 1998. The Flight Model hardware is complete and the pre-flight testing is drawing to a close. This paper examines the technical performance and capabilities of SUNSAT 1 micro satellite supporting the high resolution imager (HRI). Laboratory measured performance data are provided for the 15 m resolution 3 color CCD imager of SUNSAT, developed jointly by Stellenbosch University, the Council for Scientific Industrial Research (CSIR) in South Africa and the Korean Advanced Institute of Science and Technology (KAIST). The performance of the Attitude Determination and Control System (ADCS), which is required to support the imager, is described. -
Issue #1 – 2012 October
TTSIQ #1 page 1 OCTOBER 2012 Introducing a new free quarterly newsletter for space-interested and space-enthused people around the globe This free publication is especially dedicated to students and teachers interested in space NEWS SECTION pp. 3-22 p. 3 Earth Orbit and Mission to Planet Earth - 13 reports p. 8 Cislunar Space and the Moon - 5 reports p. 11 Mars and the Asteroids - 5 reports p. 15 Other Planets and Moons - 2 reports p. 17 Starbound - 4 reports, 1 article ---------------------------------------------------------------------------------------------------- ARTICLES, ESSAYS & MORE pp. 23-45 - 10 articles & essays (full list on last page) ---------------------------------------------------------------------------------------------------- STUDENTS & TEACHERS pp. 46-56 - 9 articles & essays (full list on last page) L: Remote sensing of Aerosol Optical Depth over India R: Curiosity finds rocks shaped by running water on Mars! L: China hopes to put lander on the Moon in 2013 R: First Square Kilometer Array telescopes online in Australia! 1 TTSIQ #1 page 2 OCTOBER 2012 TTSIQ Sponsor Organizations 1. About The National Space Society - http://www.nss.org/ The National Space Society was formed in March, 1987 by the merger of the former L5 Society and National Space institute. NSS has an extensive chapter network in the United States and a number of international chapters in Europe, Asia, and Australia. NSS hosts the annual International Space Development Conference in May each year at varying locations. NSS publishes Ad Astra magazine quarterly. NSS actively tries to influence US Space Policy. About The Moon Society - http://www.moonsociety.org The Moon Society was formed in 2000 and seeks to inspire and involve people everywhere in exploration of the Moon with the establishment of civilian settlements, using local resources through private enterprise both to support themselves and to help alleviate Earth's stubborn energy and environmental problems. -
Operational Aspects of Orbit Determination with GPS for Small Satellites with SAR Payloads Sergio De Florio, Tino Zehetbauer, Dr
Deutsches Zentrum Microwave and Radar Institute für Luft und Raumfahrt e.V. Department Reconnaissance and Security Operational Aspects of Orbit Determination with GPS for Small Satellites with SAR Payloads Sergio De Florio, Tino Zehetbauer, Dr. Thomas Neff Phone: +498153282357, [email protected] Abstract Requirements Scientific small satellite missions for remote sensing with Synthetic Taylor expansion of the phase Φ of the radar signal as a Aperture Radar (SAR) payloads or high accuracy optical sensors, pose very function of time varying position, velocity and acceleration: strict requirements on the accuracy of the reconstructed satellite positions, velocities and accelerations. Today usual GPS receivers can fulfill the 4π 233 Φ==++++()t Rtap ()()01kk apttaptt ()(-) 02030 ()(-) k aptt ()(-) k ο () t accuracy requirements of this missions in most cases, but for low-cost- λ missions the decision for a appropriate satellite hardware has to take into Typical requirements, for 0.5 to 1.0 m image resolution, on account not only the reachable quality of data but also the costs. An spacecraft position vector x: analysis is carried out in order to assess which on board and ground equipment, which type of GPS data and processing methods are most −−242 appropriate to minimize mission costs and full satisfying mission payload x≤≤⋅≤⋅ 15 mmsms x 1.5 10 / x 6.0 10 / (3σ ) requirements focusing the attention on a SAR payload. These are requirements on the measurements, not on the real motion of the satellite Required Hardware Typical Position -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 4th Quarter 1997 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 4TH QUARTER 1997 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 1st Quarter 1998 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 1ST QUARTER 1998 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
Aspects of SUNSAT Main Structure Design and Manufa
Aspects of Sunser main structure design and manufacturing fI.R. Schusterl and A.H. Basson2 (Received: January 1995; Final version May 1995) Abstract SUNSAT micro satellite project in 1989. Studies of the Department's capabilities and other programs at the uni- This paper describes sorne ouerall mechanical design 0,s- versities of Surrey and Berlin led to the January 1992 base- pects of the Stellenbosch Uniaersity satellite,'SUNSAT'. An line design compatible with Anlarup launch requirements. introduction to lhe SUNSAT project is giuen. The mechan- In 1994, NASA expressed interest in launching Sut{sar in ical design requirements are described. The design of the the same mission a^s the Danish Oersted magnetic research module trays, which conslitutes a major part of the main satellite,[2] both as secondary payloads on the Argos/Pgl- stracture, is discussed. The design and rnanufacturing of 1 Delta ll mission in October 1996. In exchange, SUNSAT the horizon sensor housing and the imager bearing hous- will provide data gathered by a precision GPS receiver ings are described to illustrate the infl,uence of the design (that NASA will supply) and the mountitrg of a set of requirements, the use of solid modelling CAD software and laser retro-reflectors on SUNSAT. The proposed orbit is the application of design fo, assembly principles in the near-polar with an inclination of 96o and an altitude vary- satellite's mechanical design. The resulting design satis- ing from 450 to 850 km.[3] firt the functional and financial constrainls. Review of previous work Introduction Thorough surveys of other international activities involv- This paper describes the mechanical design and manufac- ittg small spacecraft have been given in previous papers.[4; ture of the trays that form the main structure of Sut{sAT, 5] Only a brief summary of relevant aspects will be given as well as the horizon sensor housings and the imager bear- here. -
The Emerging Role of Cubesats for Earth Observation Applications in South Africa
Delivered by Ingenta IP: 192.168.39.151 On: Sun, 26 Sep 2021 21:03:28 Copyright: American Society for Photogrammetry and Remote Sensing The Emerging Role of Cubesats for Earth Observation Applications in South Africa Paidamwoyo Mhangara, The University of Witwatersrand PHOTOGRAMMETRIC ENGINEERING & REMOTE SENSING June 2020 333 June 2020 Layout.indd 333 5/18/2020 12:48:19 PM Introduction Cubesat technology has been augmented by a simultaneous acceleration in technological advancements in nano-, micro-, Cubesats usage is evolving from scientific demonstration and and miniature technologies in technical fields that include educational platforms to standardized space-borne scientif- telecommunications, (Opto)electronics, materials, sensors, ic instruments that support operational earth observation fluidics, and instrumentation (Woellert et al. 2011, Diaz et applications (Liebig 2000, Sandau 2010, Woellert et al. al. 2016). This technological wave enabled the development 2011, Qiao et al. 2013, Diaz et al. 2016, Kopacz et al. 2020). of a variety of miniaturized and novel autonomous instru- The effectiveness of Cubesat technology is being attested to ments and systems to facilitate remote measurements and globally as nanosatellites are increasingly used to support in- scientific experiments on a miniaturized platform. novative scientific and operational missions (Rose et al. 2012, Qiao et al. 2013, Xia et al. 2017, Poursanidis et al. 2019). Cubesats have been adopted by space agencies internationally Cubesats have long been recognized as having the potential for scientific tests and important scientific missions. Some to be a disruptive force that could replace large conventional prominent Cubesat programs include The National Aeronau- earth observation satellites (Southwood 2000, Diaz et al. -
Μc/OS-II User's Manual 1
µC/OS-II TM The Real-Time Kernel User’s Manual Jean J. Labrosse Weston, FL 33326 µC/OS-II User's Manual 1. µC/OS-II User Manual . 2 1.1 Preface . 3 1.2 Getting Started with µC/OS-II . 8 1.3 Real-Time Systems Concepts . 45 1.4 Kernel Structure . 94 1.5 Task Management . 151 1.6 Time Management . 183 1.7 Timer Management . 193 1.8 Event Control Blocks . 205 1.9 Semaphore Management . 219 1.10 Mutual Exclusion Semaphores . 235 1.11 Event Flag Management . 256 1.12 Message Mailbox Management . 285 1.13 Message Queue Management . 305 1.14 Memory Management . 333 1.15 Porting µC/OS-II . 350 1.16 80x86 Port with Emulated FP Support . 413 1.17 80x86 Port with Hardware FP Support . 460 1.18 Thread Safety of the Compiler’s Run-Time Library . 492 1.19 µC/OS-II API Reference . 500 1.20 µC/OS-II Configuration Manual . 670 1.21 PC Services . 697 1.22 C Coding Conventions . 724 1.23 Licensing Policy for µC/OS-II . 739 1.24 µC/OS-II Quick Reference . 740 1.25 TO Utility . 750 1.26 Bibliography . 752 µC/OS-II User Manual µC/OS-II User's Manual µC/OS-II User Manual This book describes the design and implementation of µC/OS-II (pronounced “Micro C O S 2”), which stands for Micro-Controller Operating System Version 2. µC/OS-II is a completely portable, ROMable, scalable, preemptive, real-time, multitasking kernel. µC/OS-II is written in ANSI C and contains a small portion of assembly language code to adapt it to different processor architectures. -
The Pcsat Mission and Cubesat Design Notes
SSC01-VIIIb-1 The PCsat Mission and Cubesat Design Notes Bob Bruninga, WB4APR, ENS Boutros, ENS Nolan, ENS Schwenzer, ENS Lawrence, LTCL B. Smith, Dr. D. Boden US Naval Academy Satellite Lab 590 Holloway Rd, Annapolis, MD 21402 [email protected] 410-293-6417 FAX 410-239-2591 Abstract There are growing opportunities for Universities to gain educational access to Space. The Naval Academy has used the Department of Defense Space Test Program for its PCsat and Sapphire projects and the Stanford Cubesat program offers a unique opportunity to get numerous small student satellite payloads into space. As a spin-off of our PCsat project, we have investigated several off-the-shelf solutions to the Telemetry, Command and control portion of small satellites that can greatly simplify small satellite and CubeSat designs. This permits students to concentrate on the various payloads and other aspects of the project without starting from scratch with a comm. system. This simple comm. System based on AX.25 packet radio is being flown this summer in the Naval Academy’s Personal Communications Satellite (PCsat) which will demonstrate downlinks receivable on Hand Held Transceivers (HT’s) with only a whip antenna. Further these simple downlinks can be easily fed into the Internet for live worldwide distribution of data. These designs are all based on the amateur radio standard on-air AX.25 packet network protocol that is implemented in a number of off-the-shelf modems (called Terminal Node Controllers or TNC’s). The following paragraphs describe three such hardware devices and the remainder of this paper describes how TNC’s and the AX.25 protocol were used on PCsat. -
CV Full Version
CURRICULUM VITAE M C Willett Name : Mike Willett Online CV at : http://vsmt.21-dc.com Address : 16011 Arenzano (GE), Italy. Poole, Dorset, BH16 5LF, England Telephone : t. +44 1212 886044 (24/7) m. +39 348 002 0847 E-mail : [email protected] Nr. of Years in Industry : 39 years Nationality : English Marital Status : Married with a son. Date of Birth : 6th October 1960 Languages : Italian and basic German. Summary of Experience I have over 30 years of embedded software experience and consider myself an expert in developing real-time embedded software using the C programming language. When I refer to real-time embedded software, I mean true multi-tasking software on a proper pre-emptive operating system with interfaces to the event driven world of hardware control and user interfaces. I have in-depth knowledge of device drivers, software control of system hardware components and product specific electro-mechanical devices. Additionally, I have a good understanding of hardware at the device level. I also have enthusiasm and expertise in requirements capture and specification. Key to any project is communication and I feel this is something that I am good at both in the written and spoken word – most importantly, I enjoy helping to bring clarity and visibility to a project, a pre- requisite for success. Specialist Skills Real-time, multi-tasking operating systems and device drivers for embedded products. Software development, firmware and 'bare metal' programming. SoCs and ASICs. Software architecture, technical auditing, project management of full product lifestyle, SW porting and reverse/re-engineering. Excellent communicator and documentation skills.