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    μ-Synthesis Control Method for Reentry Vehicle in Large Flight Envelope

    Chang, Jiang / Miao, Haochun / He, Runlin | IEEE | 2018
    This paper focuses on the application of $\mu$-synthesis theory to the tracking problem for reentry vehicle. The dynamic model for control ...

    Zero Shaping of Nonminimum Phase Aircraft Dynamics (AIAA 2018-0601)

    Caverly, Ryan / Forbes, James R. | British Library Conference Proceedings | 2018

    Zero Shaping of Nonminimum Phase Aircraft Dynamics

    Caverly, Ryan / Forbes, James R. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

    Zero miss distance of pure PNG

    Oh, Jae-Hyuk | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Zero Miss Distance Guidance Using Feedforward and Periodic Control

    Mukherjee, Dwaipayan / Ghose, Debasish | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      Zero Miss Distance Guidance Using Feedforward and Periodic Control

      Mukherjee, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Guidance , Control

    Zero-miss-distance guidance law based on line-of-sight rate measurement only

    Gurfil, Pini | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Zero-gyro control of the International Ultraviolet Explorer

    O'Donnell, James R., Jr. / Hoffman, Henry C. | NTRS | 1993
    fine sun sensor (FSS) and the two remaining gyros to provide three-axis control. A one-gyro control system that uses an additional axis of ...
    Verlag: American Institute of Aeronautics and Astronautics
    Schlagwörter: Spacecraft Design, Testing And Performance

    Zero Dynamics Analysis for Spacecraft with Fuel Slosh

    Shageer, Hesham / Tao, Gang | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

      Zero Dynamics Analysis for Spacecraft with Fuel Slosh

      Shageer, H. / Tao, G. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008
      Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.
      Schlagwörter: Guidance , Control

    Zernike moment based time sensitive targets detection and recognition

    Songzhi Jin, / Shaojun Li, / Peng Sun, et al. | IEEE | 2016
    The ground time sensitive targets have high mobility. It is hard to use traditional template matching method to detect and recognize the ...

    ZEM/ZEV Feedback Guidance Application to Fuel-Efficient Orbital Maneuvers Around an Irregular-Shaped Asteroid

    Hawkins, Matt / Guo, Yanning / Wie, Bong | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      ZEM/ZEV Feedback Guidance Application to Fuel-Efficient Orbital Maneuvers Around an Irregular-Shaped Asteroid

      Hawkins, M. / Guo, Y. / Wie, B. et al. | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Guidance , Control

    Y-Biasing: A New Operational Method for Cassini to Control Thruster Usage while Managing Reaction Wheel Momentum

    Brown, Todd | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

      Y-Biasing: A New Operational Method for Cassini to Control Thruster Usage While Managing Reaction Wheel Momentum

      Brown, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010
      Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.
      Schlagwörter: Guidance , Control , Spacecraft control , Aircraft control

    Yaw-Steered Payload Pointing and Orbital Control for a HIEO Spacecraft

    Munir, Saghir / Allison, Darcy / Machlis, Matthew et al. | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

      Yaw-Steered Payload Pointing and Orbital Control for a HIEO Spacecraft

      Munir, S. / Allison, D. / Machlis, M. et al. | British Library Conference Proceedings | 2009
      Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.
      Schlagwörter: Guidance , Control

    Yaw Guidance for Airships Under Low Airspeed Conditions

    Joos, Alexander / Fichter, Walter | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

      Yaw Guidance for Airships Under Low Airspeed Conditions

      Joos, A. / Fichter, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010
      Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.
      Schlagwörter: Guidance , Control , Spacecraft control , Aircraft control

    Yaw Dynamics Identification of an Insect-Inspired Flapping Wing Micro Air Vehicle (AIAA 2014-1468)

    Faruque, I. / Samuel, P. / Humbert, J. et al. | British Library Conference Proceedings | 2014

    XNAV Program: A New Space Navigation Architecture (AAS 06-007)

    Pines, D.J. / American Astronautical Society | British Library Conference Proceedings | 2007
    Schlagwörter: Guidance systems (Flight) , Flight control

    XNAV for Deep Space Navigation (AAS 08-054)

    Graven, P. / Collins, J. / Sheikh, S. et al. | British Library Conference Proceedings | 2008
    Schlagwörter: Guidance systems (Flight) , Flight control , Guidance , Control

    XMM-Newton: In-Orbit Performance of the AOCS (AAS 01-076)

    Elfving, A. / Pagni, V. / American Astronautical Society | British Library Conference Proceedings | 2001
    Schlagwörter: control , Rocky Mountain guidance , guidance

    XEUS Mission Dynamics Guidance and Control

    Chabot, Thomas / Udrea, Bogdan | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    XACT — A New Generation of Nano GN&C Technology (AAS 15-076)

    Hegel, Daniel / Baumgart, Matthew | British Library Conference Proceedings | 2015

    X-40A Guidance and Control and Flight Test Results (AAS 99-015)

    Nguyen, V. H. / Chaudhary, A. K. / Poladian, D. et al. | British Library Conference Proceedings | 1999
    Schlagwörter: control , Rocky Mountain guidance

    X-38 Vehicle 131R Free Flights 1, 2 & 3: FCS and Aerodynamics Lessions Learned (AAS 02-073)

    Loe, G. / Munday, S. / Hart, J. et al. | British Library Conference Proceedings | 2002
    Schlagwörter: control , guidance , Rocky Mountain guidance

    X-38 Application of Dynamic Inversion Flight Control (AAS 01-016)

    Wacker, R. / Enns, D. / Bugajski, D. et al. | British Library Conference Proceedings | 2001
    Schlagwörter: control , Rocky Mountain guidance , guidance

    X-38 Application of Dynamic Inversion Flight Control

    Wacker, Roger / Munday, Steve / Merkle, Scott | NTRS | 2001
    Control-H (MACH) is a parameterized FCS design architecture including both model-based DI rate-compensation and classical P+I command-tracking ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Stability And Control

    X-34 GNC Trades: A Simple Design for Complex Requirements (AAS 98-025)

    Osowski, T. J. / American Astronautical Society; Rocky Mountain Section | British Library Conference Proceedings | 1998
    Schlagwörter: Rocky Mountain guidance , guidance

    X-34 Auto-Landing Guidance, Navigation and Control (AAS 01-013)

    Ruth, M. / Fernandez, J. / Tracy, C. et al. | British Library Conference Proceedings | 2001
    Schlagwörter: control , Rocky Mountain guidance , guidance

    X-33 Entry Flight Control Design by Trajectory Linerization-A Singular Perturbation Approach (AAS 01-012)

    Zhu, J. J. / Hodel, A. S. / Funston, K. et al. | British Library Conference Proceedings | 2001
    Schlagwörter: control , Rocky Mountain guidance , guidance

    X-33 attitude control system design for ascent, transition, and entry flight regimes

    Hall, Charles / Gallaher, Michael / Hendrix, Neal | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

      X-33 Attitude COntrol System Design for Ascent, Transition, and Entry Flight Regimes

      Hall, C. E. / Gallaher, M. W. / Hendrix, N. D. et al. | British Library Conference Proceedings | 1998
      Schlagwörter: guidance , control

    X-33 ascent flight control design by trajectory linearization - A singular perturbation approach

    Zhu, J. / Banker, Brad / Hall, Charles | AIAA | 2000
    Verlag: The American Institute of Aeronautics and Astronautics

    X31 VECTOR Program Summary

    Young, Jennifer | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    X-31 VECTOR-ESTOL to the Ground Flight Test Results and Lessons Learned

    Grohs, Thomas / Fischer, Balazs / Heinzinger, Olaf et al. | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    WTA model study of air defense missile system based on particle algorithm

    Pengyuan, Liu / Xiong, Jiang / Wangwei, Zhang | IEEE | 2014
    In order to solve the current target distribution of large amount of calculation, and the problem of real-time computing, we propose a new ...

    Worst-Case GPS Constellation for Testing Navigation at Geosynchronous Orbit for GOES-R (AAS 13-064)

    Larson, K. / Gaylor, D. / Winkler, S. et al. | British Library Conference Proceedings | 2013
    Schlagwörter: Guidance systems (Flight) , Flight control , Control

    Worst case dynamic programming and its application to deterministic systems

    Chakravorty, Suman / Hyland, David | AIAA | 2000
    Verlag: The American Institute of Aeronautics and Astronautics

    Worst case analysis of the flight control system X-38 crew return vehicle

    Shin, Jong-Yeob / Balas, Gary / Packard, Andrew | AIAA | 1999
    Verlag: The American Institute of Aeronautics and Astronautics

    Worst Case Analysis of the Flight Control System X-38 Crew Rerum Vehicle

    Shin, J.-Y. / Balas, G. / Packard, A. et al. | British Library Conference Proceedings | 1999
    Schlagwörter: guidance

    Worst Case Analysis of a Saturated Gust Loads Alleviation System

    Knoblach, Andreas / Pfifer, Harald / Seiler, Peter J. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    WorldWide Command and Control: Operating the International Space Station

    See, M. J. / American Society for Civil Engineers; Aerospace Division | British Library Conference Proceedings | 1996

    Working-mode planning of rover in lunar exploration environment

    Hongxia, Xu / Hehua, Ju / Baofeng, Wang | IEEE | 2014
    the moving to destination, rover executes various working-modes including sensing, charging, detecting, sleeping and moving. The execution of ...

    Wolf Pack Intelligence: From Biological Intelligence to Cooperative Control for Swarm Robotics

    Hu, Jinqiang / Wu, Husheng / Zhan, Renjun | TIBKAT | 2022

    Wireless Wide Area Networked System for Navigation, Communication and Tracking

    Coleman, Norman / Lam, Ken / Papanagopoulos, George et al. | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Wireless vehicle-to-infrastructure data gathering for robot platooning

    Freier Zugriff
    Caruntu, Constantin F. / Copot, Cosmin / Lazar, Corneliu | BASE | 2017
    strategy for platoon guidance using only longitudinal changes for the automatically controlled robots. The control strategy was implemented and ...

    Wing Flexibility Induced Control Reversal For Flapping Wing Vehicles: Theoretical Analysis

    Sigthorsson, David / Oppenheimer, Michael W. / Doman, David B. et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing Flexibility Induced Control Reversal For Flapping Wing Vehicles: Observation and Evaluation

    Sigthorsson, David / Oppenheimer, Michael W. / Doman, David B. et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing Design and Testing for a Tailless Flapping Wing Micro-Air Vehicle

    Oppenheimer, Michael W. / Sigthorsson, David / Doman, David B. et al. | AIAA | 2017
    Verlag: The American Institute of Aeronautics and Astronautics

    Wingbeat Synchronization And Implementation

    Sigthorsson, David / Oppenheimer, Michael / Doman, David | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      Wingbeat Synchronization and Implementation

      Sigthorsson, D. / Oppenheimer, M. / Doman, D. et al. | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Guidance , Control

    Wind Uncertainty Correlation and Aircraft Conflict Detection Based on RUC-1 Forecasts AIAA Paper

    Chaloulos, G. / Lygeros, J. | British Library Conference Proceedings | 2007
    Schlagwörter: Guidance navigation , Guidance control

    Wind Uncertainty Correlation and Aircraft Conflict Detection Based on RUC-1 Forecasts

    Chaloulos, Georgios / Lygeros, John | AIAA | 2007
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Test Results and Performance Prediction for a Ducted Fan with Collective and Cyclic Pitch Actuation for VTOL with Efficient Cruise

    Colman, M. / Suzuki, S. / Kubo, D. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Wind Tunnel Test of an RPV with Shape-Change Effector and Sensor Arrays

    Raney, David / Cabell, Randolph / Sloan, Adam et al. | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Test of an RPV with Shape-Change Control Effector and Sensor Arrays

    Raney, David L. / Cabell, Randolph H. / Sloan, Adam R. et al. | NTRS | 2004
    and sensor networks composed of relatively small high-bandwidth devices able to simultaneously perform a variety of control functions using ...
    Verlag: NASA National Aeronautics and Space Administration

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