1–32 von 32 Ergebnissen
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Ihre Suche:
keywords:(Control

    Extended State Observer based robust attitude control of spacecraft with input saturation

    Li, Bo / Hu, Qinglei / Ma, Guangfu | Elsevier | 2015
    Schlagwörter: Control Lyapunov Function (CLF) , Optimal control

    Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation

    Shao, Xiaodong / Hu, Qinglei / Zhu, Zheng H. et al. | AIAA | 2022
    Schlagwörter: Control Moment Gyroscope , Backstepping Control , Control Algorithm , Variable Structure Control

    Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft

    Hu, Qinglei / Li, Bo / Zhang, Youmin | AIAA | 2014
    Schlagwörter: Attitude Control System , Optimal Control , Nonlinear Control

    Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation

    Hu, Qinglei / Tan, Xiao / Akella, Maruthi R. | AIAA | 2017
    Schlagwörter: Model Reference Adaptive Control , Control Algorithm , Attitude Control System , Spacecraft Control

    Observer-Based Fault Diagnosis Incorporating Online Control Allocation for Spacecraft Attitude Stabilization under Actuator Failures

    Hu, Qinglei / Li, Bo / Friswell, Michael I. | Springer Verlag | 2013
    Schlagwörter: Fault tolerant control , Control allocation

      Observer-Based Fault Diagnosis Incorporating Online Control Allocation for Spacecraft Attitude Stabilization under Actuator Failures

      Hu, Qinglei / Li, Bo / Friswell, Michael I. | Online Contents | 2013
      Schlagwörter: Control allocation , Fault tolerant control

    Tracking control of spacecraft formation flying with collision avoidance

    Hu, Qinglei / Dong, Hongyang / Zhang, Youmin et al. | Elsevier | 2014
    Schlagwörter: Adaptive control

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

    Hu, Qinglei / Ma, Guangfu | Elsevier | 2005
    Schlagwörter: Active vibration control , Variable structure control

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

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

    A composite control scheme for attitude maneuvering and elastic mode stabilization of flexible spacecraft with measurable output feedback

    Hu, Qinglei | Elsevier | 2007
    Schlagwörter: Adaptive sliding mode control (ASMC) , Vibration control

    Disturbance observer based finite-time attitude control for rigid spacecraft under input saturation

    Hu, Qinglei / Li, Bo / Qi, Juntong | Elsevier | 2014
    Schlagwörter: Finite-time control

    Robust Saturated Finite Time Output Feedback Attitude Stabilization for Rigid Spacecraft

    Hu, Qinglei / Jiang, Boyan / Friswell, Michael I. | AIAA | 2014
    Schlagwörter: Attitude Control System , Sliding Mode Control , Spacecraft Attitude Control

    Smooth finite-time fault-tolerant attitude tracking control for rigid spacecraft

    Hu, Qinglei / Shao, Xiaodong | Elsevier | 2016
    Schlagwörter: Finite time control

    Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures

    Xiao, Bing / Hu, Qinglei / Zhang, Youmin et al. | AIAA | 2014
    Schlagwörter: Feedback Control , Attitude Control System

    Decentralized Finite Time Attitude Synchronization Control of Satellite Formation Flying

    Zhou, Jiakang / Hu, Qinglei / Friswell, Michael I. | AIAA | 2012
    Schlagwörter: Nonlinear Control , Control Algorithm

    Saturated explicit reference governor for spacecraft constrained attitude reorientation control

    Chi, Biru / Hu, Qinglei | Elsevier | 2024
    Schlagwörter: Spacecraft attitude control

    Spacecraft attitude tracking control under actuator magnitude deviation and misalignment

    Hu, Qinglei / Li, Bo / Huo, Xing et al. | Elsevier | 2012
    Schlagwörter: Control allocation

    Attitude Control of Spacecraft with Actuator Uncertainty

    Hu, Qinglei / Xiao, Bing / Wang, Danwei et al. | AIAA | 2013
    Schlagwörter: Attitude Control System , Sliding Mode Control

    Kinematic Path Planning for Underactuated Spacecraft Reorientation with Forbidden Pointing Constraints

    Duan, Chao / Hu, Qinglei / Zhu, Zheng H. et al. | AIAA | 2023
    Schlagwörter: Feedback Control

    Anti-Unwinding Attitude Control of Spacecraft with Forbidden Pointing Constraints

    Hu, Qinglei / Chi, Biru / Akella, Maruthi R. | AIAA | 2018
    Schlagwörter: Attitude Control System , Model Predictive Control

    Finite-time attitude tracking control for spacecraft with uncertain actuator configuration

    Hu, Qinglei / Yu, Yanbo / Li, Bo et al. | SAGE Publications | 2015
    Schlagwörter: finite-time control

    Dynamic control allocation for spacecraft attitude stabilization with actuator uncertainty

    Zhang, Aihua / Hu, Qinglei / Huo, Xing | SAGE Publications | 2014
    Schlagwörter: control allocation

      Dynamic control allocation for spacecraft attitude stabilization with actuator uncertainty

      Zhang, Aihua / Hu, Qinglei / Huo, Xing | Tema Archiv | 2014
      Schlagwörter: control allocation

    Dual-Quaternion-Based Spacecraft Autonomous Rendezvous and Docking Under Six-Degree-of-Freedom Motion Constraints

    Dong, Hongyang / Hu, Qinglei / Akella, Maruthi R. | AIAA | 2017
    Schlagwörter: Model Predictive Control , Adaptive Output Feedback Control

    Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault

    Hu, Qinglei / Tan, Xiao / Akella, Maruthi R. | AIAA | 2017
    Schlagwörter: Proportional Integral Derivative Control , Aircraft Flight Control

    Attitude cooperative control of spacecraft formation via output-feedback

    Lv, Yueyong / Hu, Qinglei / Ma, Guangfu et al. | Emerald Group Publishing | 2012
    Schlagwörter: Cooperative attitude control

    Spacecraft Attitude Reorientation with Reaction Wheel Assembly via State-Dependent Coefficient Parameterizations

    Yao, Junyu / Hu, Qinglei / Zheng, Jianying et al. | AIAA | 2022
    Schlagwörter: Pseudospectral Optimal Control

    Saturated Attitude Control for Rigid Spacecraft Under Attitude Constraints

    Hu, Qinglei / Liu, Yueyang / Dong, Hongyang et al. | AIAA | 2020
    Schlagwörter: Feedback Control

    Safety Control for Spacecraft Autonomous Rendezvous and Docking Under Motion Constraints

    Dong, Hongyang / Hu, Qinglei / Akella, Maruthi R. | AIAA | 2017
    Schlagwörter: Adaptive Control Method

    New Impact Time and Angle Guidance Strategy via Virtual Target Approach

    Hu, Qinglei / Han, Tuo / Xin, Ming | AIAA | 2018
    Schlagwörter: Linear Quadratic Control Problem

    Reaction Wheel Fault Compensation and Disturbance Rejection for Spacecraft Attitude Tracking

    Xiao, Bing / Hu, Qinglei / Singhose, William et al. | AIAA | 2013
    Schlagwörter: Attitude Control System

    Adaptive Pose Tracking Control for Spacecraft Proximity Operations Under Motion Constraints

    Dong, Hongyang / Hu, Qinglei / Liu, Yueyang et al. | AIAA | 2019
    Schlagwörter: Model Predictive Control