1–16 of 16 hits
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    Control allocation for spacecraft under actuator faults

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | TIBKAT | 2021

    Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    Introduction

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    Conclusions

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    Fault-tolerant attitude control of spacecraft

    Hu, Qinglei / Xiao, Bing / Li, Bo et al. | TIBKAT | 2021

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

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    Mathematical Model of the Attitude Control System

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

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

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    Extended State Observer Based Optimal Attitude Robust Control of Spacecraft

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021

    Robust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment

    Hu, Qinglei / Li, Bo / Xiao, Bing et al. | Springer Verlag | 2021