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Robust adaptive attitude tracking control with L2 -gain performance and vibration reduction of an or
  • ISSN号：0022-0434
  • 期刊名称：Journal of Dynamic Systems Measurement and Control
  • 时间：2011.1.1
  • 页码：1-9
  • 相关项目：航天器执行器故障的输出反馈容错控制研究
作者： Qinglei Hu|
同期刊论文项目
航天器执行器故障的输出反馈容错控制研究
期刊论文 55 会议论文 3
同项目期刊论文
Fault-tolerant attitude control for flexible spacecraft without angular velocity magnitude measureme
L-2 Disturbance Attenuation Control for Input Saturated Spacecraft Attitude Stabilization without An
Spacecraft attitude tracking control under actuator magnitude deviation and misalignment
Robust finite-time control allocation in spacecraft attitude stabilization under actuator misalignme
基于反步法与动态控制分配的航天器姿态机动控制
基于反步法的主从航天器相对姿态控制
控制受限的卫星轨道转移过程中的姿态控制
基于有向图的航天器编队鲁棒自适应姿态协同跟踪控制
基于广义逆的欠驱动航天器姿态机动控制
考虑执行器安装偏差时航天器姿态稳定的控制分配
与自由翻滚目标近距离段交会对接的相对姿轨耦合控制
过驱动航天器飞轮故障重构与姿态容错控制
Intelligent proportional-derivative control for flexible spacecraft attitude stabilization with unkn
Fault-tolerant control with H∞ performance for attitude tracking of flexible spacecraft
Adaptive sliding mode fault tolerant attitude tracking control for flexible spacecraft under actuato
Adaptive nonlinear proportional-derivative type fault tolerant control for flexible spacecraft attit
Robust attitude control design for spacecraft under assigned velocity and control constraints
Adaptive fault tolerant control using integral sliding mode strategy with application to flexible sp
Fault tolerant attitude stabilization control for spacecraft with actuator saturation
Attitude tracking compensation control for rigid spacecraft under actuator misalignment and fault
Input-to-state stable attitude control for rigid spacecraft with actuator faults and misalignments
Active fault tolerant attitude control for flexible spacecraft with loss of actuator effectiveness
Reaction wheel fault tolerant control for spacecraft attitude stabilization with finite-time converg
考虑推力器安装偏差的航天器姿态机动有限时间控制
考虑执行器安装偏差的航天器姿态稳定与控制分配
Finite-time fault tolerant attitude control for over-activated spacecraft subject to actuator misali
Adaptive integral-type sliding mode control for spacecraft attitude maneuvering under actuator stuck
推力器故障的刚体航天器自适应变结构容错控制
基于观测器的航天器执行机构失效故障重构
航天器执行机构部分失效故障的鲁棒容错控制
执行器故障的挠性航天器姿态滑模容错控制
Robust fault tolerant control for spacecraft attitude stabilization under actuator faults and bounde
Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiv
基于新型终端滑模的航天器执行器故障容错姿态控制
带时变通信时间延迟的卫星编队姿态协同自适应L_2增益控制
卫星编队飞行输出反馈姿态协同跟踪控制
考虑执行机构误差的编队卫星姿态分布式时延滑模自适应协同控制
应用SGCMG的卫星姿态快速机动控制
基于协同进化粒子群和Pareto最优解的卫星编队队形重构方法
基于微分平滑的欠驱动刚性航天器时间最优轨迹规划研究
深空环境下卫星编队飞行队形重构实时重规划
欠驱动航天器姿态调节滑模控制
空间机器人终端滑模路径跟踪控制
带卡尔曼估计器的无拖曳卫星干扰补偿控制
自由漂浮柔性空间机器人轨迹跟踪控制
Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures
基于一致性算法的卫星编队姿轨耦合的协同控制
执行器卡死并失效的航天器姿态稳定控制
有向图中网络Euler-Lagrange系统的自适应协调跟踪
多星系统相对轨道的自适应协同控制
Delay Depending Decentralized Adaptive Attitude Synchronization Tracking Control of Spacecraft Formation
欠驱动航天器实时最优控制算法设计
含时变时延的卫星编队姿态协同自适应滑模L2增益控制