| 引用本文: | 杨希祥,张家实.风场中平流层飞艇轨迹跟踪的滑模控制方法.[J].国防科技大学学报,2019,41(1):1-4.[点击复制] |
| YANG Xixiang,ZHANG Jiashi.Sliding mode control for trajectory tracking of stratospheric airships in wind field[J].Journal of National University of Defense Technology,2019,41(1):1-4[点击复制] |
|
| |
|
|
| 本文已被：浏览 7209次 下载 7111次 |
| 风场中平流层飞艇轨迹跟踪的滑模控制方法 |
| 杨希祥1,2, 张家实1 |
|
(1. 国防科技大学 空天科学学院， 湖南 长沙 410073;2.
2. 湖北航天技术研究院 总体设计所， 湖北 武汉 430034)
|
| 摘要: |
| 为实现平流层飞艇驻空阶段可控飞行，研究环境风场中横侧向轨迹跟踪的滑模控制方法。建立平流层飞艇驻空阶段动力学模型，将动力学方程解耦为纵向运动方程和横侧向运动方程，采用小扰动方法对动力学方程进行线性化；利用滑模控制对外部干扰强鲁棒的特性，设计横侧向轨迹跟踪的滑模控制器；以直线与圆组成的复合轨迹跟踪控制为例，对提出的轨迹控制方法进行仿真验证。仿真结果表明，所提基于滑模的轨迹跟踪控制方法鲁棒性好，在一定范围的风场扰动条件下，可以实现对指令轨迹的有效跟踪控制，响应特性好。 |
| 关键词: 平流层飞艇 轨迹跟踪 滑模控制 |
| DOI：10.11887/j.cn.201901001 |
| 投稿日期：2018-04-02 |
| 基金项目:国家自然科学基金资助项目（11102229）;湖南省自然科学基金资助项目（2018JJ3590） |
|
| Sliding mode control for trajectory tracking of stratospheric airships in wind field |
| YANG Xixiang1,2, ZHANG Jiashi1 |
|
(1. College of Aeronautics and Astronautics, National University of Defense Technology, Changsha 410073, China;2.
2. Institute of Overall Design, Hubei Academy of Spaceflight Technology, Wuhan 430034, China)
|
| Abstract: |
| In order to realize the controllable flight of stratospheric airships during floating, the sliding mode control for lateral trajectory tracking in wind field was researched. The dynamic models of the stratospheric airship during floating were established, and the models were linearized by using linear perturbation theory. The sliding mode controller for lateral trajectory tracking was designed. Considering that this method was insensitive to external perturbation, the trajectory tracking for linear formation and circular was simulated. Simulation results show that the robustness and response characteristic of the trajectory tracking method based on sliding mode control are both satisfactory, and the control accuracy is high in wind field. |
| Keywords: stratospheric airship trajectory tracking sliding mode control |
|
|
