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  • 1
    ISSN: 1573-7527
    Keywords: autonomous robots ; agent architectures ; action selection and planning ; diagnosis ; integration and coordination of multiple activities ; fault protection ; operations ; real-time systems ; modeling
    Source: Springer Online Journal Archives 1860-2000
    Topics: Computer Science , Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract This paper describes the New Millennium Remote Agent (NMRA) architecture for autonomous spacecraft control systems. The architecture supports challenging requirements of the autonomous spacecraft domain not usually addressed in mobile robot architectures, including highly reliable autonomous operations over extended time periods in the presence of tight resource constraints, hard deadlines, limited observability, and concurrent activity. A hybrid architecture, NMRA integrates traditional real-time monitoring and control with heterogeneous components for constraint-based planning and scheduling, robust multi-threaded execution, and model-based diagnosis and reconfiguration. Novel features of this integrated architecture include support for robust closed-loop generation and execution of concurrent temporal plans and a hybrid procedural/deductive executive. We implemented a prototype autonomous spacecraft agent within the architecture and successfully demonstrated the prototype in the context of a challenging autonomous mission scenario on a simulated spacecraft. As a result of this success, the integrated architecture has been selected to fly as an autonomy experiment on Deep Space One (DS-1), the first flight of NASA';s New Millennium Program (NMP), which will launch in 1998. It will be the first AI system to autonomously control an actual spacecraft.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2013-08-31
    Description: The problem of acquiring a simple but sufficiently accurate model of a dynamic system is made more difficult when the dynamic system of interest is a multibody system comprised of several components. A low order system model may be created by reducing the order of the component models and making use of various available multibody dynamics programs to assemble them into a system model. The difficulty is in choosing the reduced order component models to meet system level requirements. The projection and assembly method, proposed originally by Eke, solves this difficulty by forming the full order system model, performing model reduction at the the system level using system level requirements, and then projecting the desired modes onto the components for component level model reduction. The projection and assembly method is analyzed to show the conditions under which the desired modes are captured exactly; to the numerical precision of the algorithm.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: Proceedings of the 3rd Annual Conference on Aerospace Computational Control, Volume 2; p 778-791
    Format: application/pdf
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  • 3
    Publication Date: 2019-01-25
    Description: The Cassini Attitude and Articulation Control Subsystem (AACS) is responsible for determining and controlling the spacecraft attitude including instrument pointing, antenna pointing, and thrust vector pointing during velocity change maneuvers. The 12 year mission life, long round-trip light time, and extended periods of coast without continuous ground control drive the AACS flight software design in the directions of autonomy, fault tolerance, and modularity to accommodate planned upgrades in flight. The Cassini AACS Flight Software is depicted in increasing levels of detail using a Context Diagram, Architecture Diagrams (i.e., Dependency Diagrams), an Object Diagram for each object, and a Statechart (i.e., State Transition Diagram) for each object. The detail contained in the diagrams is enhanced and refined during the Requirements and Design Phases of both Subsystem and Software Development. Examples of all the diagrams as well as the criteria for object selection, the advantages of statecharts, and the ease of modifying the design to accommodate changes in scope are described.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: (ISSN 0065-3438); sic Space Science; U
    Format: text
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  • 4
    Publication Date: 2019-07-13
    Description: Conference topics included definition of tool requirements, advanced multibody component representation descriptions, model reduction, parallel computation, real time simulation, control design and analysis software, user interface issues, testing and verification, and applications to spacecraft, robotics, and aircraft.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: NASA-CR-186446 , JPL-PUBL-89-45-VOL-1 , NAS 1.26:186446 , Nov 01, 1989; Oxnard, CA; United States
    Format: application/pdf
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  • 5
    Publication Date: 2019-07-13
    Description: This volume of the conference proceedings contain papers and discussions in the following topical areas: Parallel processing; Emerging integrated capabilities; Low order controllers; Real time simulation; Multibody component representation; User environment; and Distributed parameter techniques.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: NASA-CR-186447 , JPL-PUBL-89-45-VOL-2 , NAS 1.26:186447 , Nov 01, 1989; Oxnard, CA; United States
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