. "Satellite Platforms And Payloads, Space Mission"@en . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Fundamentals of space missions"@en . . "7.5" . "Why Space?, Exploring Space, Space Mission Analysis, Space Environment, Orbital Mechanics, Mission and Operation Design, Communication Link Analysis, Launch Vehicles, The Business of Space" . . "Hybrid"@en . "TRUE" . . "Fundamentals of satellite systems and subsystems"@en . . "7.5" . "Payload and Spacecraft Design, On-Board Data Systems, Attitude and Orbit Control Systems, Communication Systems, Propulsion Systems, Thermal and Electrical Power Systems, Mechanics of Materials" . . "Hybrid"@en . "TRUE" . . "Satellite communications"@en . . "7.5" . "On-Board Signal Processing, Signal Propagation, RF Modelling and Design Tools, RF Measurement, Characterization and Calibration Techniques, RF Devices" . . "Hybrid"@en . "TRUE" . . "Management Issues of space systems and missions"@en . . "7.5" . "Missions and Operations Design, Launch Vehicles, Project Management, PA/QA, Space Market, Space Policy and Law" . . "Hybrid"@en . "FALSE" . . "Space missions and operations design"@en . . "7.5" . "Not provided" . . "Hybrid"@en . "TRUE" . . "Science and exploration missions"@en . . "3" . "Introduction to completed and planned space missions:\r\nExamples are (i) Gravity Probe A for testing the gravitational redshift, (ii) Gravity Probe \r\nB for testing the gravitomagnetic Schiff effect, (iii) Cassini for Saturn exploration and \r\ntesting the gravitational time delay, (iv) Pioneer for planetary exploration and testing \r\nthe gravitational field in the Solar system, (v) MICROSCOPE for testing the \r\nEquivalence Principle, (vi) LISA for searching for gravitational waves and the \r\ntechnology mission LISA pathfinder, (vii) GRACE and GRACE-FO for satellite based \r\ngeodesy, (viii) ACES on the ISS for testing relativity and establishing space-based\r\nmetrology, (ix) further missions testing Special and General Relativity using quantum \r\noptics, (x) asteroid and comet missions HAYABUSA and Rosetta. For each mission the \r\nrequirements on the payload technology, the spacecraft technology, and on the \r\nmission scenario will be derived.\n\nOutcome:\nParticipants are able to discuss science cases for space and exploration missions, \r\nmeasurement schemes and payload as well as technology requirements on payload \r\nand mission." . . "Presential"@en . "TRUE" . . "Mission design"@en . . "1.5" . "Availabe: General Module (Space Flight Theory) Description\n•Trajectory computation and space flight analysis\n•Basic principles for designing and analysing a space mission\n\nOutcome: General Module (Space Flight Theory) Outcomes\nStudents have knowledge/responsibilities in:\n•Space mission analysis and design (tools)\n•Orbital and attitude dynamics\n•Modeling approaches of space environment\n•Satellite system modeling (thermal, sensors, actuators)\n•Definitions and technical terms of space applications and optimization\n•Mathematical models and problem statements relating to space applications\n•Using mathematical software\n•Numerical solution of mathematical problems" . . "Presential"@en . "TRUE" . . "Mission analysis"@en . . "3" . "Availabe: General Module (Space Flight Theory) Description\n•Trajectory computation and space flight analysis\r\n•Basic principles for designing and analysing a space mission\r\n\nOutcome: General Module (Space Flight Theory) Outcomes\nStudents have knowledge/responsibilities in:\r\n•Space mission analysis and design (tools)\r\n•Orbital and attitude dynamics\r\n•Modeling approaches of space environment\n•Satellite system modeling (thermal, sensors, actuators)\r\n•Definitions and technical terms of space applications and optimization\r\n•Mathematical models and problem statements relating to space applications\r\n•Using mathematical software\r\n•Numerical solution of mathematical problems" . . "Presential"@en . "TRUE" . . "Scientific payloads"@en . . "3" . "No Description, No Learning Outcome" . . "Presential"@en . "FALSE" . . "Research and exploration missions"@en . . "3" . "No Description, No Learning Outcome" . . "Presential"@en . "FALSE" . . "Satellite communications and security"@en . . "5" . "This course will cover the fundamentals of satellite communications. Starting from system architecture and constellations, we study the satellite spectrum, channel and link budgets. A digital communications primer is included with complementary laboratory exercises, along with a detailed analysis of communication payloads. Finally, a series of current topics are covered, such as standards and security, integration with 5G, satellite IoT and deep space scientific missions. \n\nOutcome:\nThe students will be able to study and understand: · the SatCom system architecture and constellations · the satellite spectrum and its implications in SatCom services · the satellite channel characteristics and link budgets · latest digital communication techniques for SatComs · the various architectures and capabilities of SatCom payloads · relevant standards and security aspects · integration of satellite systems within the 5G ecosystem · Internet of Things services over satellite · Comm aspects of deep space scientific missions" . . "Presential"@en . "TRUE" . . "design and analysis of satellite missions"@en . . "6" . "no data" . . "Presential"@en . "TRUE" . . "fixed and mobile satellite communication systems"@en . . "5" . "no data" . . "Presential"@en . "FALSE" . . "global navigation satellite systems basics and applications"@en . . "4" . "no data" . . "Presential"@en . "FALSE" . . "Satellite systems"@en . . "5" . "no data" . . "Presential"@en . "FALSE" . . "Satellite systems"@en . . "5" . "no data" . . "Presential"@en . "FALSE" . . "Global navigation satellite systems"@en . . "3" . "The goal of the course is to introduce students with Global Navigation Satellite Systems and their applications. Tasks of the course, that include acquisition of knowledge, skills and competences are: 1) to acquire knowledge about GNSS working principles, 2) to learn basic GNSS data processing workflows, 3) identify shortcomings and advantages of GNSS, 4) to obtain competences in practical applications of GNSS. The course is being studied in Latvian.\r\nCourse responsible lecturer\tZaiga Krišjāne\r\nResults\tKnowledge; 1.Describe theoretical background of GNSS. 2.Are familiar with data processing methods in the field of GNSS. 3.Characterize GNSS measurement workflow and error estimations. Skills 4.Know how to work with GNSS equipment. 5.Know how to process obtained measurements. 6.Are able to quantify precision and accuracy of the measurements. Competencies 7.Select most suitable GNSS measurement method for solution of specific problem. 8.Integrate GNSS measurements in preparation of geospatial information." . . "Presential"@en . "FALSE" . . "Spacecraft subsystems and space mission design"@en . . "6" . "In the first part of the course, the student acquires fundamentals on systems engineering of space systems and the key aspects of spacecraft systems design. He/she will also learn the design considerations which come into play in laying out a space mission and its preliminary design. In the second part of the course, students are taken step-by-step through the complete process of creating and evaluating multiple methods for reducing space mission cost and schedule and critically evaluate alternative ways of achieving mission objectives at dramatically lower cost and in much less time." . . "no data"@en . "FALSE" . . "Introduction to satellite systems"@en . . "10" . "Students get an understanding of satellite systems and their applications, physical properties of the space environment and the systems engineering elements of a spacecraft project. This course gives the students the basics for further studies within aerospace technology." . . "Presential"@en . "FALSE" . . "Global navigation satellite systems"@en . . "5" . "Accurate and reliable positioning has become increasingly important for the navigation of vehicles, drones and autonomous systems. Global satellite-based positioning systems play a key role in fulfilling that need.\n\nThe course aims to give a solid knowledge about global navigation satellite systems, how the systems work, and how accurate positions may be obtained. In addition, the course provides a good knowledge of the mathematical modelling principles used for both code and phase-based GNSS positioning (GPS, Galileo, or Glonass) and the integration with other types of navigation sensors." . . "Presential"@en . "FALSE" . . "Satellites and launcher systems"@en . . "8" . "explain the structure and operation of a rocket;\ndevelopment of the first prototypes to the development of flight models;\ndesign, build, test, and calibrate space-compatible instruments" . . "Presential"@en . "TRUE" . . "Space mission design"@en . . "10.00" . "This is a design study for an astronomical spacecraft which takes usually place at La Laguna University (ULL), Tenerife, Spain. It is likely that the trip will take place remotely in 2020/2021. The focus of this module is to carry out a design study for an astronomical spacecraft mission with instrumentation for the detection of gamma-rays from astrophysical sources.\n\nThe students make use of lectures, tutorials, computer and library facilities to assemble a review of the state of knowledge for such a proposed instrumentation challenge. They then work in parallel in teams of students. The aim is to produce a well thought-out spacecraft design for a specific gamma-ray astrophysics goal, after a concentrated period of intensive work.\n\nA series of approximately 12 lectures will be given in UCD prior to the trip, in order to provide students with the necessary basic technical skills required for undertaking the study. Students will be required to perform an extensive review of current gamma-ray missions and to review the literature in relation to science goals in high energy astrophysics.\n\nAdvisors will be available to assist the student teams with various aspects of their task. For example, they would provide support in such areas as: computation, detector design, astrophysics, mission planning and the environment of space. Each team will be directly supervised by a member of staff from either UCD, Southampton or ULL. Depending on numbers, this field trip may not run in every academic year. This trip takes place in late March/early April.\n\nLearning Outcomes:\nOn completion of this module students will be able to:\n- work in small teams with each member having a specific responsibility, and know how to interact positively with other members of a close team,\n- perform a detailed of the relevant literature\n- devise a solution to a complicated problem in a relatively short period of time,\n- work closely with people from a different country and background,\n- write software pipelines in a suitable language (e.g. Python) for the simulation of spacecraft instrument performance and sensitivity\n- develop presentation and research skills\n- prepare a mission feasibility study\n- present scientific results comprehensively and fluently, orally and in writing" . . "Presential"@en . "TRUE" . . "Basic course in satellite operations"@en . . "3.00" . "Learning outcomes\nIn the basic satellite operation course, students are trained in the operation of TU Berlin satellites. With successful completion of the\nAfter the final examination, they receive a license to operate satellites independently under supervision and within the framework of the regulations Possibilities.\n\nTeaching content\n\n• Basic orbit mechanics and orbit propagation (“Why do the satellites come to Berlin when and for how long?”)\n• Redundancy as a guiding principle for the safe development of space systems\n• Basics of amateur radio\n• Overview of the BEESAT-2 and -4 satellites and their subsystems\n• Ground station architecture of the TU Berlin and its radio link\n• Telecommand and telemetry structure of BEESATs\n• Introduction to the operating programs TM-Viewer, TC-Control and TM-Analyzer and support software (gpredict and others.)\n• Basic operating procedures (“NOP”, telemetry and image download, reset)\n• Complex operational procedures (commanders, imaging, attitude control and GPS experiments)" . . "Presential"@en . "FALSE" . . "Satellite operations project"@en . . "6.00" . "Learning outcomes\n\nIn the satellite operation project, students are trained in the operation of the TU Berlin satellites. With successful completion of the\nIntermediate examination you will receive a license to operate satellites independently under supervision and within the framework of the regulations Possibilities. In advanced project work, what has been learned is directly applied to improve knowledge of satellite operations and thus...\nDeeper understanding of space systems.\n\nTeaching content\n\n• Basic orbit mechanics and orbit propagation (“Why do the satellites come to Berlin when and for how long?”)\n• Redundancy as a guiding principle for the safe development of space systems\n• Basics of amateur radio\n• Overview of the BEESAT-2 and -4 satellites and their subsystems\n• Ground station architecture of the TU Berlin and its radio link\n• Telecommand and telemetry structure of BEESATs\n• Introduction to the operating programs TM-Viewer, TC-Control and TM-Analyzer and support software (gpredict and others.)\n• Basic operating procedures (“NOP”, telemetry and image download, reset)\n• Complex operational procedures (commanders, imaging, attitude control and GPS experiments)\n\nDifferent aspects of satellite operations are dealt with in depth in project topics that change every semester. Become there addresses various interdisciplinary target groups" . . "Presential"@en . "FALSE" . . "Satellite communication (satcom)"@en . . "6.00" . "Learning Outcomes\nSatellite communication is an essential part of all satellite missions. The numerous small satellites of TU Berlin offer a unique insight into\nthis field. In the scope of this curricular project, the participants build ground station components within interdisciplinary teams. The course\ncovers topics from radio communication and signal processing as well as electrical, mechanical and software engineering. Students will be\nable to summarize the working principles of hardware and software related to satellite communication. In combination with the knowledge\nand skills gained in other courses in space and electrical engineering, the participants will be able to set up a a satellite communication link.\nThey will document and present their work at the end of the project.\nAfter successful completion of this module, students will be able to\n- work in an interdisciplinary project team,\n- describe the general structure of satellite ground stations as well as their hard- and software components,\n- organize small aerospace engineering projects,\n- use open source soft- and hardware tools for management and development,\n- recognize basic terms relevant for satellite communication,\n- explain the architecture of a satellite link,\n- use equipment for measuring the quality of a satellite link.\nContent\n- Applied technical know-how regarding satellite communications: e.g. characteristics of electromagnetic waves, components for transmitter\nand receiver circuits, antennas, transmission path, modulation and encoding schemes, operating modes, EMC, electronics, mechanics,\nprogramming, networking and other IT components etc.\n- Practical hardware and/or software design as well as manufacturing and implementation\n- Using electrical and RF measuring instruments and/or troubleshooting tools\n- Methods for planning and organizing projects\n- Technical and project documentation and presentation of the practical work" . . "Presential"@en . "FALSE" . . "Satellite design"@en . . "12.00" . "Learning outcomes\n\nThe module teaches the basics and methods for designing satellites. All segments of a space flight mission\nand in particular the design of subsystems is discussed in more detail. The students should all subsystems in one Satellite bus and the satellite system, ie the connection of the satellite bus to the payload, can be designed and developed\nTeaching content\nThe content of the satellite design module covers the following subject areas:\n\nPlanning a satellite mission\nDerivation of requirements for the satellite design\nDesign concepts and satellite types\nSubsystem design\nSystem integration design\nSystem engineering\nPlanning system verification\n." . . "Presential"@en . "FALSE" . . "Space mission analysis"@en . . "6.00" . "Learning outcomes\nThe Space Mission Analysis module is aimed at students with a particular interest in mission design and analysis\nStudents with a general desire to work in the space sector. The module follows on from the space flight mechanics course and\noffers, on the one hand, application of the content learned there and, on the other hand, practical in-depth study. The course is one of the basics an LRT Masters focused on space travel.\n\nAfter successful completion, students are able to:\n- Formulate mission design-specific requirements\n- Practical application of knowledge from the space flight mechanics module\n-- Programming and parameterization of orbit propagation\n-- Calculation of orbit maneuvers\n-- corresponding visualizations\n- to create a basis for decision-making for an optimal orbit choice\n-- Identification of design drivers\n-- Calculation of the crucial parameters\n-- Trade-off analysis\n- to determine the orbit of a satellite\n-- Analysis of historical data\n-- Orbit determination based on historical data\n-- Differentiation between orbit determination methods in terms of their informative value\n- carry out basic calculations on satellite constellations\n\nThe goal in the end is to obtain an independently developed tool for mission analysis, which uses parameterization for used for a variety of missions and can be further expanded. Programming is done using MATLAB.\n\nTeaching content\n\nThe course covers the following subject areas\n- Basics of space flight mechanics\n- Design of a satellite mission\n-- Mission requirements\n-- Mission phases (launch, transfer, nominal)\n- Orbital design\n-- Orbit types\n-- Orbit design parameters\n-- Trade-offs\n- Methods of orbit determination\n- Design of satellite constellations\n-Transfer\n-- types\n-- Design and calculation" . . "Presential"@en . "FALSE" . . "Space mission planning and operations"@en . . "6.00" . "Learning Outcomes\nThe space industry is demanding systems engineers who are capable of planning a space mission from project initiation to completion. This\nmodule introduces the programmatic aspects of space mission planning and operations. This involves acquiring a robust knowledge on the\ninternational standards and activities in astronautics. One focus of the module is set on gaining competencies in planning a space mission\nthrough its whole life cycle. Another focus is set on mission operations, which covers the theoretical aspects of ground stations and mission\ncontrol structures, as well as handling procedures for mission operations.\nAfter successful completion of this module, students will be able to\n- identify the main elements of space mission planning and operations (e.g. user and mission concept analysis, data processing, archiving\nand distribution),\n- explain the design steps to plan a space mission from project initiation to completion,\n- apply the design steps of space mission planning on a project,\n- develop a systematic approach to plan a project following international standards,\n- justify design choices from a programmatic point of view,\n- assess the feasibility of a space project,\n- recognize the relevance of space laws in mission planning,\n- select software tools that support the execution of space mission planning,\n- describe the European space program (e.g. agencies, budgets, activities, facilities),\n- explain the principles of creating a mission operations concept,\n- recognize the main elements of a ground station,\n- describe the traditional RF-telecommunication chain from ground to space, and vice versa.\nContent\n- Basics of space mission planning\n- Introduction to ECSS standards\n- Space activities of ESA, DLR, CNES\n- Basics of space operations\n- Satellite operations\n- Regulatory aspects for space missions (space law)\n- Ground station architectures\n- Tools for space mission planning\n- Project on mission design" . . "Presential"@en . "FALSE" . . "Satellite systems and communication"@en . . "10,5" . "Basics of communication satellites, calculation of geostationary orbit; structure of the communications engineering payload, the mechanical and electrical subsystems of a satellites. modulation procedures for satellite communications" . . "Presential"@en . "FALSE" . . "Space missions and systems"@en . . "9.0" . "Provide basic knowledge on the design of space missions, and on spacecraft navigation and attitude control.\nAbility to dimension and design simple systems for orbit and attitude determination and control.\nKnowledge of space mission phases and operations." . . "Presential"@en . "TRUE" . . "Conceptual design of a space mission"@en . . "3.0" . "Educational goals\n\nThe course aims to develop the creative thinking of space and astronautical engineering students through the definition, at an architectural level, of a space mission aimed at specific objectives provided by the teachers. Students will achieve the educational objective in a team work activity by making use of the methodologies, skills, notions and computational tools acquired during the first year of the master's degree. In order to achieve the educational goals, concurrent engineering tools may be used. The activity will end up in the production of a \"Concept Document\" which will contain the solution proposed by each team to achieve the mission objectives. Assembling the Concept Document will provide the students with the ability to carry out an efficient bibliographic research, aimed at obtaining the required information in the published literature, fact sheets of instrumentation and subsystems, and, if necessary, via a direct request to potential suppliers. The drafting of the \"Concept Document\" in the standard form of a mission pre-proposal, through the organic presentation of the proposed solution, the selection and detailing of the most important aspects, the highlighting of critical issues, will conclude the group work activity. In summary, the learning objectives of the course can be listed as follows:\n\ndevelopment of creative thinking through the definition, at an architectural level, of a space mission aimed at specific objectives;\nacquisition of the ability to organize the methodologies, skills, notions and calculation tools acquired during the first year of the master's degree towards the conceptual definition of a space mission, through a team-work activity;\nlearning how an efficient bibliographic search is carried out, aimed at acquiring information available in the literature, on fact sheets of instriments and subsystems, and direct interaction with potential suppliers;\nacquisition of the ability to summarize the work carried out effectively, consistently and concisely, through the writing of a Concept Document.\n\n\nThe Concept Document will offer a creative, yet viable, solution of a central problem of space engineering (the conceptual design of a space mission), starting from the skills all courses of the Astronautical and Space Engineering. This creative project will be carried out in groups, stimulating mutual comparisons and fostering the communication skills of the students." . . "Presential"@en . "TRUE" . . "Engineering design of space missions and spacecraft components"@en . . "5.0" . "Aims: \n\nUpon completion of this course, the student is able to:\n\nunderstand and explain the orbital mechanics and dynamics of space missions in general and for specific applications;\nunderstand and explain what the main environmental constraints are on the functioning of technology in space;\nunderstand and explain how launchers and space systems (plattforms and payload) are designed to meet the specific conditions of the space environment;\nunderstand and explain how interdisciplinary crosstalk between science, technology development, and societal aspects is essential for the scientific exploitation and exploration of space.\n\nModule 2.5 ects. Orbital Mechanics and Mission Design (2.5 ECTs)\n\nIntroduction\n\nOverview and classification of space missions\n\n\nOrbital mechanics\n\nfundamental laws in kinematics and dynamics (Keplerian orbits, types of orbits,orbital parameters)\nmaneuvers (acceleration and deceleration for in in-plane maneuvers, maneuvers for plane change\nthe central body\nclassification of orbits for space missions\nSpacecraft systems\n\nattitude and orbital control system\npower generation and management\nthermal control\nspacecraft structure\ntelemetry\ncommunications\nLaunch vehicles and launch trajectories\n\nlaunch site\nlaunch trajectory\nlaunch vehicle\nintegration with spacecraft\nMission design\n\nspecification of mission objectives\nexamples of space missions\n\nModule Spacecraft Design and Instrumentation (2.5 ECTs)\n\nGeneral outline\n \nSpacecraft definition and characteristics\nSpace environment and constraints\nMechanical and thermal engineering\nAssembly, Integration, Testing and Verification\nObservation and science mission payloads\n \nDetailed contents\n \nSpace messengers (gravity, magnetic field, photons, particles, dust, samples, gravitational waves)\nWhy space activities and orbit selection.\nSpace segments\n\nOn ground environment\nLaunch environment\nSpace environment and impacts on the design of spacecraft and instrumentation\n- Radiative environment, thermal cycling\n- Vacuum, outgassing\n- Microgravity\n- Contamination\n- Residual atmosphere in Low Earth Orbit, atomic oxygen and drag\n- Radiations\n- Meteorites and orbital debris\n- Electrical environment (solar wind, magnetosphere, radiation belts, plasma environment)\n- Energetic particles, electrons, protons and ions\n- Electrical charge of the spacecraft\nEffects on the optical, mechanical and thermal design, ageing of components.\n\nMechanical and dynamical design of instruments\nThermal design of instruments\nThermal control\nMaterial properties and material selection criteria\nCommunication with and inside the spacecraft\nOn-board software\nData reduction and compression\nRedundancy concepts\nDifferent steps in the design of space instruments\nContamination and cleanliness, on the ground and in space\nElectromagnetic compatibility\nAssembly, Integration, Tests, Verification\nGround Support Equipment\nModel philosophy\nMission Planning\nQualification of instruments\nCalibration of instruments\nEuropean Cooperation for Space Standardization (ECSS) standards\nMeasurement strategies: remote sensing vs in situ; active vs passive\nDetectors: principles, noise properties and constraints on observing modes\n\nMore information at: https://onderwijsaanbod.kuleuven.be/syllabi/e/G0S56AE.htm#activetab=doelstellingen_idp834864" . . "Presential"@en . "TRUE" .