1–20 von 35 Ergebnissen
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    Nonlinear decoupling sliding mode control and attitude control of spacecraft

    Singh, S.N. / Iyer, A. | Tema Archiv | 1989
    Schlagwörter: VARIABLE STRUCTURE SYSTEMS , VARIABLE-STRUCTURE-CONTROL , ORBITING SPACECRAFT

    Co-operative oscillations of bubbles (space cryogenics)

    Snyder, H.A. / Mord, A.J. | Tema Archiv | 1990
    Schlagwörter: SPACECRAFT STRUCTURE

    The Galileo Orbiter: command and telemetry subsystems on their way to Jupiter

    Erickson, J.K. | Tema Archiv | 1990
    Schlagwörter: SPACECRAFT CLOCK , SUBCOMMUTATED STRUCTURE

    Robust decentralized control laws for the ACES structure

    Collins, E.G. jun. / Phillips, D.J. / Hyland, D.C. | Tema Archiv | 1991
    Schlagwörter: ACES STRUCTURE , ACTIVE CONTROL TECHNIQUE EVALUATION FOR SPACECRAFT

    Development of the MiniSIL™ structural design

    Aglietti, G S / Wicks, A / Barrington-Brown, A J | SAGE Publications | 1999
    Schlagwörter: spacecraft testing , structure

    A hybrid control scheme of adaptive and variable structure for flexible spacecraft

    Li, Zhi-Bin / Wang, Zhao-Lin / Li, Jun-Feng | Elsevier | 2004
    Schlagwörter: Flexible spacecraft , Variable structure control

    Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver

    Hu, Qinglei / Ma, Guangfu | Elsevier | 2005
    Schlagwörter: Flexible spacecraft , Variable structure control

    Variable Structure Output Feedback Control of a Spacecraft Under Input Dead-Zone Non-Linearity

    Hu, Q | SAGE Publications | 2007
    Schlagwörter: flexible spacecraft , variable structure control

    The thermal environment encountered in space by a multifunctional solar array

    Foster, J.A. / Aglietti, G.S. | Elsevier | 2009
    Schlagwörter: Multifunctional structure , Spacecraft

    Nonlinear optimal control of spacecraft approaching a tumbling target

    Xin, Ming / Pan, Hejia | Elsevier | 2010
    Schlagwörter: Spacecraft , Flexible structure

    Mission analysis and performance comparison for an Advanced Solar Photon Thruster

    Dachwald, Bernd / Wurm, Patrick | Elsevier | 2011
    Schlagwörter: Inflatable structure , Gossamer spacecraft

    Hybrid thrusters and reaction wheels strategy for large angle rapid reorientation with high precision

    Ye, Dong / Sun, Zhaowei / Wu, Shunan | Elsevier | 2012
    Schlagwörter: Spacecraft attitude tracking , Variable structure control

    Review of hardware cost estimation methods, models and tools applied to early phases of space mission planning

    Trivailo, O. / Sippel, M. / Şekercioğlu, Y.A. | Elsevier | 2012
    Schlagwörter: Cost Breakdown Structure , Product Breakdown Structure , Spacecraft/Vehicle Level Cost Model , Work Breakdown Structure

    A Designing Method of Variable Topology-Transformable Spacecraft

    Ning, Xin / Yue, Xiao Kui | Trans Tech Publications | 2013
    Schlagwörter: Structure Dynamics , Variable Topology-Transformable Spacecraft

    Attitude Error Kinematics

    Younes, Ahmad Bani / Mortari, Daniele / Turner, James D. et al. | AIAA | 2013
    Schlagwörter: Spacecraft Tracking , Variable Structure Control , Spacecraft Attitude

    Stability of relative equilibria of the full spacecraft dynamics around an asteroid with orbit–attitude coupling

    Wang, Yue / Xu, Shijie / Zhu, Mengping | Elsevier | 2013
    Schlagwörter: Full spacecraft dynamics , Non-canonical Hamiltonian structure

    Real-Time Nonlinear Attitude Control System for Nanosatellite Applications

    Li, Junquan / Post, Mark / Lee, Regina | AIAA | 2013
    Schlagwörter: Spacecraft Attitude , Variable Structure Control

    Spacecraft Anti-Unwinding Attitude Control with Actuator Nonlinearities and Velocity Limit

    Hu, Qinglei / Li, Li / Friswell, Michael I. | AIAA | 2015
    Schlagwörter: Spacecraft Performance , Spacecraft Attitude , Variable Structure Control

    Passivity-Based Adaptive Finite-Time Trajectory Tracking Control for Spacecraft Proximity Operations

    Sun, Liang | AIAA | 2015
    Schlagwörter: Target Spacecraft , Variable Structure Control