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    Characterizing Observed Limit Cycles in the Cassini Main Engine Thrust Vector Control System

    Rizvi, F. / Weitl, R. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Engine Yaw Augmentation for Hybrid-Wing-Body Aircraft via Optimal Control Allocation Techniques

    Taylor, B. / Yoo, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Flight Implementation of Pseudospectral Optimal Control for the TRACE Space Telescope

    Karpenko, M. / Bhatt, S. / Bedrossian, N. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Finite-Horizon Optimal Control Using Neural Networks with an Application to Orbit Transfer Problems

    Heydari, A. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Application of H-infinity Fault Diagnosis to ADDSAFE Benchmark: the Control Surface Jamming Case

    Marcos, A. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Optimal Control Modification Adaptive Law with Covariance Adaptive Gain Adjustment and Normalization

    Nguyen, N. / Burken, J. / Hanson, C. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Effect of Control Surface-Fuselage Inertial Coupling on Hypersonic Vehicle Flight Dynamics

    Falkiewicz, N. / Frendreis, S. / Cesnik, C. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Optimal Control Applied to Aircraft Longitudinal Axis for Energy Trajectory Recovery

    Lefebvre, M. / Constans, F. / Berard, C. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Singularity Visualization and Steering Control Law of Adaptive Skew Pyramid Type CMGs

    Kojima, H. / Matsuda, N. / Yamaguchi, S. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    On Time Delay Margin Estimation for Adaptive Control and Robust Modification Adaptive Laws

    Nguyen, N. / Summers, E. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Longitudinal Dynamics and Adaptive Control Application for an Aeroelastic Generic Transport Model

    Nguyen, N. / Tuzcu, I. / Yucelen, T. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Real-time pattern recognition for guidance of an autonomous undersea submersible

    Nguyen, H.G. / Heckman, P.J. jun. / Pai, A.L. | Tema Archiv | 1988
    Fast vision algorithms on compact and imbeddable hardware are developed for the guidance and control of an autonomous underwater vehicle ...

    Multi-satellite control system architecture and mission scheduling optimization

    Jung-Hyun, Lee / Myung, Wang Se / Chung, Daewon et al. | IEEE | 2012
    In this paper we propose an architecture for multi-satellite control systems and an optimization procedure for mission operations. The ...

    Phase Synchronization Control of Robotic Networks on Periodic Ellipses with Adaptive Network Topologies

    Chung, S. / Chang, I. / Hadaegh, F. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Research on Modeling and Control Strategy of Contra-Rotating Open Rotor Engine

    Chen, Fengping / Chen, Yuchun | IEEE | 2022
    matching of the core engine and CRP. The generation method of optimal CRP working point can provide guidance for the control law design of CRP in ...

    Derivative-Free Output Feedback Adaptive Control of an Aeroelastic Generic Transport Model

    Yucelen, T. / Calise, A. / Kim, K. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Dynamics and Optimal Control for Free-Flight and Tethered Arrays in Low Earth Orbit

    Mazouz, Rayan / Quadrelli, Marco / Beauchamp, Robert | IEEE | 2021
    corrections to maintain stability. To fly optimal paths and keep communications with the Deep Space Network minimal, autonomous Guidance, Navigation ...

    Experimental Model Based Robust Aeroservoelastic Control for the S^4T Wind-Tunnel Model

    Zeng, J. / Moulin, B. / Kukreja, S. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Experimental Study on Combining a Simple Input Shaper and Adaptive Positive Position Feedback Control

    Orszulik, R. / Shan, J. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    A Piloted Evaluation of Damage Accommodating Flight Control Using a Remotely Piloted Vehicle

    Cunningham, K. / Cox, D. / Murri, D. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Accounting for Performance Limitations Inside the Model Following Control System of an Unmanned Helicopter

    Klussendorf, F. / Lorenz, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Flight Test of Composite Model Reference Adaptive Control (CMRAC) Augmentation Using NASA AirSTAR Infrastructure

    Gregory, I. / Gadient, R. / Lavretsky, E. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Robust controllers based on feedback linearization for automated lane guidance of heavy vehicles

    Tai, M. / Tomizuka, M. | Tema Archiv | 2000
    control, and the other among the line of sliding mode control. In either approach, the idea of feedback linearization is utilized to deal with ...

    Fault-Tolerant Control for Unmanned Surface Vehicles with Digital Communication Channel

    Chen, Liheng / Fu, Shasha / Zhao, Yuxin | TIBKAT | 2022

    A spreader acceleration guidance scheme for command guided surface-to-air missiles

    Ghose, D. / Dam, B. / Prasad, U.R. | Tema Archiv | 1989
    of the proposed guidance law in comparison with existing laws in terms of integral control effort, interception time, and miss distance. The ...
    Schlagwörter: COMMAND AND CONTROL SYSTEMS , SPREADER ACCELERATION GUIDANCE , GUIDANCE LAW

    Cassini at Saturn Proximal Orbits - Attitude Control Challenges

    Burk, Thomas A. | NTRS | 2013
    control team deals with radiation hazards. The angular size and unique geometry of the rings and Saturn near periapsis means that star ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Lunar And Planetary Science And Exploration

    Attitude Determination and Control Subsystem (ADCS) Preparations for the EPOXI Flyby of Comet Hartley 2

    Luna, M. / Collins, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Aerodynamic and Thrust Force Modeling for a Propulsion Assisted Control Aircraft Test Bed

    Merceruio, Z. / Phillips, K. / Gu, Y. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Experiments with a Passivity-based Formation Control System for Teams of Small Robotic Drones

    Rabbath, C. / Lechevin, N. / Apkarian, J. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    HUD Guidance for the ASKA Experimental STOL Aircraft using Radar Position Information

    Yazawa, Kenji / Terui, Yushi / Hardy, Gordon H. | NTRS | 1992
    The paper describes a high performance HUD guidance system installed on the experimental powered-lift STOL aircraft Aska. Since the maiden ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Communications And Navigation

    Cable Angle Feedback Control Systems to Improve Handling Qualities for Helicopters with Slung Loads

    Ivler, C. / Tischler, M. / Powell, J. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Geometric 3D Path-Following Control for a Fixed-Wing UAV on SO(3)

    Cichella, V. / Xargay, E. / Dobrokhodov, V. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Comparison of Periodic System Lifting Techniques for Robust Stability Analysis of Magnetic Spacecraft Attitude Control Systems

    Lohr, J. / Winkler, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Investigation of Active Vibration Suppression of a Flexible Satellite using Magnetic Attitude Control

    Findlay, E. / Forbes, J. / Liu, H. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Design of Launch Vehicle Flight Control Systems Using Ascent Vehicle Stability Analysis Tool

    Jang, J. / Alaniz, A. / Hall, R. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    (AAS 20-104) Altitude Control of a Solar Balloon for Mars Exploration

    Schuler, Tristan / Shkarayev, Sergey / Thangavelautham, Jekan | TIBKAT | 2020

    Underwater glider motion control

    Mahmoudian, N. / Woolsey, C. | Tema Archiv | 2008
    convergent path following. This paper describes the dynamic modelling of the complete multi-body control system and the development and numerical ...

    Suppression of the Aeroelastic/Aeroservoelastic Interaction Using Adaptive Feedback Control Instead of Notching Filters

    Zeng, J. / Wang, J. / De Callafon, R. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Flight Control for a Class of 155 mm Spin-stabilized Projectiles with Course Correction Fuse (CCF)

    Theodoulis, S. / Wernert, P. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    UAV path generation, path following and gimbal control

    Sun, Meirui / Zhu, Rongming / Yang, Xueguang | Tema Archiv | 2008
    to UAV location, and then gives the guidance law of the path following system of UAV and the gimbal tracking way. The results of computer ...

    Design and analysis of lunar lander manual control modes

    Duda, Kevin R. / Johnson, Michael C. / Fill, Thomas J. | IEEE | 2009
    proposed during Apollo, are reviewed and discussed in terms of their applicability to Altair. The ALHAT guidance, navigation, and control (GNC ...

      Design and analysis of lunar lander manual control modes

      Duda, K.R. / Johnson, M.C. / Fill, T.J. | Tema Archiv | 2009
      proposed during Apollo, are reviewed and discussed in terms of their applicability to Altair. The ALHAT guidance, navigation, and control (GNC ...

    Attitude control system performance of RCA Satcom

    MUHLFELDER, L. | AIAA | 1976
    Verlag: The American Institute of Aeronautics and Astronautics

    Adaptive Output Feedback Control of the NASA GTM Model with Unknown Nonminimum-Phase Zeros

    D Amato, A. / Sumer, E. / Mitchell, K. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Virtual Development and Validation of a Function for an Automated Lateral Control using Artificial Neural Networks and Genetic Algorithms

    Liu-Henke, Xiaobo / Yarom, Or Aviv / Scherler, Soeren | IEEE | 2020
    In this paper the development of a function for an automated lateral guidance by means of a consistently model-based and verification ...

    Drag modulation flight control for aerocapture

    Putnam, Zachary R. / Clark, Ian G. / Braun, Robert D. | IEEE | 2012
    studies by extending the analysis of single-event jettison systems to Earth and Mars. A single-event jettison guidance algorithm was developed and ...

    Adaptive Output Feedback Control for an Aeroelastic Generic Transport Model: A Parameter Dependent Riccati Equation Approach

    Kim, K. / Calise, A. / Yucelen, T. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Impact of Plume Modeling on the Design and Control for a Class of Air-Breathing Hypersonic Vehicles

    Sridharan, S. / Dickeson, J. / Rodriguez, A. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    The Effect of Faster Engine Response on the Lateral Directional Control of a Damaged Aircraft

    May, R. / Lemon, K. / Csank, J. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Considerations for the application of a route guidance system in the Greater Toronto Area

    Blum, Y. / Van Aerde, M. / Case, E.R. | Tema Archiv | 1989
    The feasibility of applying a route guidance system of the Q-route type is examined, and some system design aspects that one would have to ...
    Schlagwörter: TRAFFIC COMPUTER CONTROL , ROUTE GUIDANCE SYSTEM , TRAFFIC CONTROL CENTRES

    Robust Trajectory and Attitude Control of a Flexible Launcher

    Bernelli-Zazzera, F. / European Space Agency | British Library Conference Proceedings | 2003
    Schlagwörter: spacecraft guidance , control systems

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