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Comments on “Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking
  • ISSN号：0278-0046
  • 期刊名称：IEEE Transactions on Industrial Electronics
  • 时间：2013
  • 页码：2771-2773
  • 相关项目：基于非光滑控制的飞行器制导控制问题研究
作者： Kemao Ma|
同期刊论文项目
基于非光滑控制的飞行器制导控制问题研究
期刊论文 30 会议论文 10
同项目期刊论文
Global finite-time stabilization design for a class of high-order uncertain nonlinear systems
Guidance law implementation with performance recovery using an extended high-gain observer
高精度制导律的非光滑设计与实现
具有单框架控制力矩陀螺航天器的建模及可控性分析
On stability and application of extremum seeking control without steady-state oscillation
高阶滑模制导律的设计与实现
Controllability analysis and attitude path planning of underactuated spacecraft systems
Cooperative guidance laws with constraints on impact time and terminal angle
不确定非线性系统的非光滑控制及应用
大型空间飞行器的高阶滑模姿态控制律设计
登月舱上升段最优轨迹设计
采用直接力的空空导弹越肩发射控制设计
航天器连续非光滑姿态控制律设计
Spacecraft maneuvers via singularity-avoidanceof SGCMGs Based on DMPC
Improved backstepping control for large angle maneuvers of spacecraft
Design and comparison ofLQR and a novel robust backstepping controller for supercavitating vehicles
欠驱动航天器飞轮控制方法
不同攻角约束下空空导弹敏捷转弯过程弹道优化
空空导弹敏捷转弯的分段线性滑模控制设计
Global finite-time stabilization design for a class of high-order uncertain nonlinear systems