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000857355 019__ $$a932593502$$a936352430$$a985046821$$a1005761847$$a1011847922$$a1026458518$$a1048172429$$a1066477990
000857355 020__ $$a9783319235035$$q(electronic book)
000857355 020__ $$a3319235036$$q(electronic book)
000857355 020__ $$z3319235028
000857355 020__ $$z9783319235028
000857355 0247_ $$a10.1007/978-3-319-23503-5$$2doi
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000857355 050_4 $$aTL795.4
000857355 08204 $$a629.43/4$$223
000857355 24504 $$aThe FLP microsatellite platform :$$bflight operations manual /$$cJens Eickhoff, editor.
000857355 264_1 $$aCham :$$bSpringer,$$c[2016]
000857355 264_4 $$c©2016
000857355 300__ $$a1 online resource (xxvi, 680 pages) :$$billustrations..
000857355 336__ $$atext$$btxt$$2rdacontent
000857355 337__ $$acomputer$$bc$$2rdamedia
000857355 338__ $$aonline resource$$bcr$$2rdacarrier
000857355 347__ $$atext file$$bPDF$$2rda
000857355 4901_ $$aSpringer aerospace technology,$$x1869-1730
000857355 504__ $$aIncludes bibliographical references and index.
000857355 5050_ $$aIntro; Foreword; Preface; Donation for Life; Contents; Contributors; Abbreviations; 1 Introduction to the Microsatellite Platform; 2 The FLP Platform Operability; 3 Data Handling and Control Concept; 4 Core Data Handling Subsystem; 5 Power Supply Subsystem; 6 Platform Communication Subsystem; 7 Attitude Control Subsystem; 8 Thermal Control Subsystem; 9 Payload Control Subsystem ; 10 Failure Detection, Isolation and Recovery Concept; 11 Satellite Mission Phases and Planning; 12 Stuttgart Mission Control Infrastructure ; 13 Stuttgart/DLR Infrastructure for LEOP.
000857355 5058_ $$a14 Earth Observation Mission Planning15 Flight Procedures; 16 FLP Mission Information Database; 17 Annexes and Data Sheets; References; Index; Abstract; 1.1 The University Small Satellite Program; 1.2 Satellite Orbit; 1.3 Mechanical Design and Launcher Interface; 1.4 Technology and Payloads; 1.5 Platform Re-usability; 1.6 Platform Redundancy Concept; 1.7 Power Subsystem and Electrical Block Diagram; 1.8 Core Data Handling Subsystem; 1.9 FLP Payload Control Computer; 1.10 Attitude Control Subsystem; 1.11 Reaction Control Subsystem; 1.12 Communication Subsystem; 1.13 Thermal Control Subsystem.
000857355 5058_ $$a1.14 Satellite Deorbiting at End of Life1.15 Possible Mechanical Platform Configurations; Abstract; 2.1 Spacecraft Configuration Handling Concept; 2.2 Spacecraft Telecommand and Telemetry Structure; 2.3 Application Process ID Definitions (APIDs); 2.4 PUS Tailoring Concept; 2.5 Spacecraft Commandability and Observability; 2.6 Spacecraft On-board Time Management; Abstract; 3.1 Onboard Software Architecture; 3.2 OBSW Object Types; 3.3 Observability Functions Provided by the OBSW; 3.4 FLP Software Dynamic Architecture; 3.5 Onboard Software Death Report; Abstract.
000857355 5058_ $$a4.1 On-Board Data Handling Subsystem4.2 Combined Data and Power Management Infrastructure; 4.3 Data Management; 4.4 System Boot at Launcher Separation; 4.5 OBSW Controlled Functions; 4.6 Core DHS Subsystem Control; Abstract; 5.1 Subsystem Overview; 5.2 Solar Panels; 5.3 Solar Array Deployment Mechanism; 5.4 Battery; 5.5 Power Control and Distribution Unit; 5.6 Power Subsystem Control; Abstract; 6.1 TTC Subsystem Overview; 6.2 Signal Acquisition Procedure; 6.3 TTC Subsystem Control; Abstract; 7.1 Subsystem Overview; 7.2 Mission Objectives and ACS Subsystem Modes; 7.3 Magnetometers.
000857355 5058_ $$a7.4 Sun Sensor Unit7.5 GPS Receiver System; 7.6 Fiberoptic Gyroscopes; 7.7 Star Tracker; 7.8 Reaction Wheels; 7.9 Magnetotorquers; 7.10 Extensions for FLP Generation 2; 7.11 ACS Subsystem Control; Abstract; 8.1 Thermal Subsystem Overview; 8.2 Sensors, Calibration, Limits; 8.3 TCS Subsystem Control; Abstract; 9.1 Aspects of Payload Control and Data Handling; 9.2 Payload Control on the First FLP Based Satellite; 9.3 Payload Control in Network-Centric Architectures; Abstract; 10.1 General Principles; 10.2 Core DHS FDIR; 10.3 Power FDIR; 10.4 Equipment FDIR; 10.5 TTC FDIR; 10.6 ACS FDIR.
000857355 506__ $$aAccess limited to authorized users.
000857355 520__ $$aThis book represents the Flight Operations Manual for a reusable microsatellite platform - the "Future Low-cost Platform" (FLP), developed at the University of Stuttgart, Germany. It provides a basic insight on the onboard software functions, the core data handling system and on the power, communications, attitude control and thermal subsystem of the platform. Onboard failure detection, isolation and recovery functions are treated in detail. The platform is suited for satellites in the 50-150 kg class and is baseline of the microsatellite "Flying Laptop" from the University. The book covers the essential information for ground operators to controls an FLP-based satellite applying international command and control standards (CCSDS and ECSS PUS). Furthermore it provides an overview on the Flight Control Center in Stuttgart and on the link to the German Space Agency DLR Ground Station which is used for early mission phases. Flight procedure and mission planning chapters complement the book.
000857355 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed December 22, 2015).
000857355 650_0 $$aArtificial satellites$$xControl systems.
000857355 650_0 $$aMicrospacecraft.
000857355 7001_ $$aEickhoff, Jens,$$eeditor.
000857355 77608 $$iPrint version:$$z9783319235028
000857355 830_0 $$aSpringer aerospace technology.
000857355 852__ $$bebk
000857355 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-3-319-23503-5$$zOnline Access$$91397441.1
000857355 909CO $$ooai:library.usi.edu:857355$$pGLOBAL_SET
000857355 980__ $$aEBOOK
000857355 980__ $$aBIB
000857355 982__ $$aEbook
000857355 983__ $$aOnline
000857355 994__ $$a92$$bISE