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    Application of multivariable design techniques to robust control of a large-scale system

    Hammett, K.D. / Dowdle, J.R. / Athans, M. et al. | Tema Archiv | 1991
    Typical issues and tradeoffs resulting from application of various modern multivariable controller design techniques to large-scale systems ...
    Verlag: American Institute of Aeronautics and Astronautics , Washington

    Optimization of magnetic attitude and angular momentum control for low earth orbit satellites

    Bals, J. / Fichter, W. / Surauer, M. | Tema Archiv | 1997
    The control system design for a three axis stabilized bias momentum satellite is discussed. The satellite is equipped with one pitch ...

    An approach to network based criteria in longitudinal control of vehicle platoons

    Maschuw, J.P. / Keßler, G.C. / Abel, D. | Tema Archiv | 2007
    This paper presents a control analysis for wireless network supported longitudinal guidance of platoons with a limited number of vehicles ...

    An overview on aerospatiale mangnetic bearing products for spacecraft attitude control and for industry

    Samuel, A. / Lechable, B. | Tema Archiv | 1997
    magnets and on the control of the rotor around a zero force equilibrium point The present paper recalls the cronology of magnetic Bearing history ...

    LQG control design for a hovering micro air vehicle using an optical tracking system

    Hendrix, C.D. / Veth, M.J. / Carr, R.W. | Tema Archiv | 2009
    The need to conduct warfare in urban environments presents a new frontier for navigation and control of UAV's in locations where GPS may be ...

    A new approach for CHAMP safe mode attitude control

    Bauer, H. / Schmitt, C. | Tema Archiv | 1997
    After a short overview of the CHAMP satellite and its AOCS a new approach for safe mode attitude control, using simply a 2-axis sun sensor ...

    Drag-free & attitude control system for the gravity explorer mission

    Vaillon, L. / Champetier, C. | Tema Archiv | 1997
    This paper has presented the preliminary definition of the Drag-Free and Attitude Control System (DFACS) for the GOCE mission, as performed ...

    Effect of Choice of Basis Functions in Neural Network for Capturing Unknown Function for Dynamic Inversion Control

    Ramesh, Gandham / Dwivedi, P.N. / Naveen Kumar, P. et al. | Tema Archiv | 2013
    The basic requirement for an autopilot is fast response and minimum steady state error for better guidance performance. The highly ...

    Design of a microcontroller based state control for a magnetic levitation transport system

    Groning, I. / Butz, S. / Henneberger, G. | Tema Archiv | 1998
    only needs a simple and cheap track for levitation and guidance. The vehicle is stabilised by a state control scheme. Loading and unloading is ...
    Verlag: Institute of Electrical and Electronics Engineers (IEEE) , New York

    Passage simulation of monorail suspension conveyors and transport goods for collision prevention

    Wunderlich, Thomas A. / Schäfer, Thomas / Auer, Stefan | Tema Archiv | 2008
    Modern industrial production involves complex and time-critical process chains which demand a sophisticated supply chain management and ...

    Symbolic derivation of open-loop dynamic models of multibody mechatronic systems for control purpose. A case study: The LISA technology package

    Da Lio, M. / Bortoluzzi, D. | Tema Archiv | 2003
    symbolic mathematical models produced in this way are suitable to form "plant models" that may be exploited for the design of control systems. In ...

    Flight controller design for intercepting missiles with multiple TVC systems and DCS

    Lin, I-Fan / Huang, Chin-I / Fu, Li-Chen | Tema Archiv | 2007
    missiles: guidance law (GL) and autopilot is presented. The GL is designed with dynamic sliding mode control (DSMC) to eliminate the chattering ...

    Path-following algorithms and experiments for an autonomous surface vehicle

    Bibuli, Marco / Caccia, Massimo / Lapierre, Lionel | Tema Archiv | 2007
    guidance laws either at kinematic and dynamic level. The proposed nonlinear Lyapunov- based control law yields convergence of the path following ...

    An Energy-Aware Airborne Dynamic Data-Driven Application System for Persistent Sampling and Surveillance

    Frew, Eric W. / Argrow, Brian / Houston, Adam et al. | Tema Archiv | 2013
    processes for onboard data and dynamic atmospheric models that assimilate Doppler radar data; and iii.) a hierarchical guidance and control ...

    Complete Equipment Inspection Method Based on Risk Assessment and Nondestructive Testing

    Huang, Hui / Chen, Ding-Yue / Mao, Guo-Jun et al. | Tema Archiv | 2013
    Three propylene spherical tanks which have both the same manufacturing parameters and conditions have been assessed based on risk ...

    Description and applications for an automated inertial azimuth measuring system

    Shearer, J.A. / Atwill, W.D. | Tema Archiv | 1978

    Performance of a ring laser strapdown attitude and heading reference for aircraft

    Giovanni, C.S. | Tema Archiv | 1978

    Attitude and heading reference system I-AHRS for the EFIGENIA autonomous unmanned aerial vehicles UAV based on MEMS sensor and a neural network strategy for attitude estimation

    Cordoba, M.A. | Tema Archiv | 2007
    For the autonomous flight, navigation, guidance and control of the EFIGENIA unmanned aerial vehicle it is essential to have high ...

    Star sensors and harsh environment

    Berrighi, G. / Procopio, D. | Tema Archiv | 2003

    Autonomous precision landing and hazard detection and avoidance technology (ALHAT)

    Epp, C.D. / Smith, T.B. | Tema Archiv | 2007
    landing Guidance, Navigation and Control (GNC) hardware and software technologies necessary for these capabilities. The ALHAT project will qualify ...

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