| 引用本文: | 孙启超,徐娟娟,张焕水.高超声速飞行器再入轨迹跟踪的块压缩模型预测控制方法[J].控制理论与应用,2026,43(4):814~820.[点击复制] |
| SUN Qi-chao,XU Juan-juan,ZHANG Huan-shui.Block condensing model predictive control for reentry trajectory tracking of hypersonic vehicle[J].Control Theory & Applications,2026,43(4):814~820.[点击复制] |
|
| 高超声速飞行器再入轨迹跟踪的块压缩模型预测控制方法 |
| Block condensing model predictive control for reentry trajectory tracking of hypersonic vehicle |
| 摘要点击 159 全文点击 21 投稿时间:2024-01-31 修订日期:2024-12-20 |
| 查看全文 查看/发表评论 下载PDF阅读器 HTML |
| DOI编号 10.7641/CTA.2024.40089 |
| 2026,43(4):814-820 |
| 中文关键词 高超声速飞行器 轨迹跟踪 模型预测控制 块压缩 序列二次规划 |
| 英文关键词 hypersonic vehicles trajectory tracking model predictive control block-condensing sequential quadratic programming |
| 基金项目 国家自然科学基金创新研究群体项目(61821004)资助. |
|
| 中文摘要 |
| 本文针对高超声速飞行器的再入轨迹跟踪控制问题, 考虑了非线性模型预测控制的计算加速方法. 首先采
用序列二次规划算法, 将非线性最优控制问题转化为迭代差值的线性最优控制问题, 再应用块压缩方法, 将长时域
问题转化为多段较短区间内的最优控制问题. 利用对偶特性推导了由拉格朗日乘子优化问题和分段最优控制问题
组成的双层迭代结构. 由于拉格朗日乘子迭代优化, 相邻的最优问题解耦, 可以并行计算. 最后, 对控制和拉格朗日
乘子同时进行热启动, 减少迭代次数, 提高求解速度. 仿真结果显示, 在保证控制效果的前提下, 控制器求解速度显
著提高. |
| 英文摘要 |
| In this paper, a computational acceleration method for nonlinear model predictive control is considered to
track trajectories for the reentry of hypersonic vehicles. First, a sequential quadratic programming algorithm is adopted to
transform the nonlinear optimal control problem into a linear optimal control problem with iterative differences. Then, a
block condensing method is applied to transform the long horizon problem into an optimal control problem with multiple
short intervals. The principle of duality is exploited to derive a two-layer iterative structure that consist of a Lagrange
multiplier optimization problem and segmented optimal control problems. As the nearby optimal problems is decoupled
by the iterative optimized Lagrange multiplier, they are computed in parallel. Finally, the control and Lagrange multipliers
are warm-started simultaneously to reduce the number of iterations and improve the solution speed. The simulation results
show that the solving speed of the controller is significantly enhanced while maintaining the effective control performance. |