| 引用本文: | 赖爱芳,郭毓,郑立君.航天器姿态机动及稳定的自抗扰控制[J].控制理论与应用,2012,29(3):401~407.[点击复制] |
| LAI Ai-fang,GUO Yu,ZHENG Li-jun.Active disturbance rejection control for spacecraft attitude maneuver and stability[J].Control Theory and Technology,2012,29(3):401~407.[点击复制] |
|
| 航天器姿态机动及稳定的自抗扰控制 |
| Active disturbance rejection control for spacecraft attitude maneuver and stability |
| 摘要点击 2212 全文点击 1624 投稿时间：2011-05-24 修订日期：2011-08-18 |
| 查看全文 查看/发表评论 下载PDF阅读器 |
| DOI编号 10.7641/j.issn.1000-8152.2012.3.CIAC110594 |
| 2012,29(3):401-407 |
| 中文关键词 航天器 自抗扰控制 扩张状态观测器 快速机动 高稳定度 |
| 英文关键词 spacecraft active disturbance rejection control extended state observer fast maneuver high stability |
| 基金项目 国家自然科学基金资助项目(60975075); 空间智能控制技术国家重点实验室资助项目. |
|
| 中文摘要 |
| 针对航天器动力学参数不确定性以及系统存在外部持续干扰的问题, 提出了一种自抗扰姿态控制器的设计方法. 在为期望姿态安排过渡过程的基础上, 设计了扩张状态观测器, 对参数不确定性和外部干扰进行估计, 并实时补偿. 为抑制跟踪误差, 设计了非线性状态误差反馈律. 仿真结果表明, 该控制器不仅能很好地估计并补偿系统受到的持续干扰, 而且对航天器动力学参数的不确定性具有较强的鲁棒性, 满足航天器姿态快速机动和高稳定度的控制要求, 性能指标明显优于PD控制. |
| 英文摘要 |
| For a spacecraft with dynamic parametric uncertainties and external persistent disturbances, we present an active disturbance rejection control (ADRC). After arranging the transient dynamics of the desired attitude, we design an extended state observer (ESO) to estimate the impact from parametric uncertainties and disturbances, and realize corresponding compensations online. A nonlinear state error feedback law is designed to reject the tracking error. Simulation results show that the designed controller not only accurately estimates and compensates the persistent disturbances, but also realizes the robustness to dynamic parametric uncertainties of the spacecraft. It meets the requirements on the spacecraft fast attitude maneuver and high stability. The performance indices are much superior to those of the PD controller. |
|
|
|
|
|