| 引用本文: | 张杨,吴文海,胡云安,程春华.舰载无人机着舰轨迹跟踪鲁棒控制器设计[J].控制理论与应用,2018,35(4):557~565.[点击复制] |
| ZHANG Yang,WU Wen-hai,HU Yun-an,CHENG Chun-hua.Design of landing trajectory tracking robust controller for carrier-based unmanned aerial vehicle[J].Control Theory and Technology,2018,35(4):557~565.[点击复制] |
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| 舰载无人机着舰轨迹跟踪鲁棒控制器设计 |
| Design of landing trajectory tracking robust controller for carrier-based unmanned aerial vehicle |
| 摘要点击 2354 全文点击 1246 投稿时间：2017-03-21 修订日期：2017-12-09 |
| 查看全文 查看/发表评论 下载PDF阅读器 |
| DOI编号 10.7641/CTA.2017.70179 |
| 2018,35(4):557-565 |
| 中文关键词 舰载无人机 纵向控制 轨迹跟踪 受限指令 预设性能 |
| 英文关键词 carrier-based unmanned aerial vehicles longitudinal control trajectory tracking constrained command prescribed performance |
| 基金项目 国家自然科学基金项目(60674090, 51505491), 中国博士后科学基金(2015M572693)资助. |
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| 中文摘要 |
| 为确保舰载无人机着舰阶段精确地跟踪下滑轨迹, 并且在稳态性能基础上具有更好的瞬态性能, 本文在新
的等效误差模型的基础上提出了受限指令预设性能控制律设计方法. 首先考虑了舵面受限和角速率受限等实际工
程问题, 引入受限指令滤波方法, 然后综合考虑建模误差和外界扰动, 引入了连续的双曲正切函数对饱和函数进行
近似, 并设计了自适应律对模型未知参数进行估计, 最后引入了预设性能方法对着舰的瞬态性能进行了重点分析.
通过理论推导和仿真验证, 证明了本文提出的方法在复杂着舰环境下有较好的瞬态性能和较好的鲁棒性. |
| 英文摘要 |
| The carrier-based unmanned aerial vehicle (UAV) should be required to track the trajectory accurately and
ensured to have the transient performance during landing. And in this paper a constrained command prescribed control law
based on a new equivalent error model is designed. Firstly, a constrained command filter method is introduced to consider
the actual engineering problems such as rudder limited and angular rate limited. Secondly, the continuous hyperbolic
tangent function is used to approximate the saturation function, and an adaptive law is used to estimate the unknown
parameters with the modeling errors and a variety of environmental disturbance factors. Finally, the transient performance
during landing is emphatically analyzed by introducing prescribed performance method. The strong robustness and better
transient performance in complex environment is demonstrated by theoretical analysis and simulation. |
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