收稿日期:
2023-03-30
修回日期:
2023-04-27
接受日期:
2023-05-16
出版日期:
2023-08-15
发布日期:
2023-05-18
通讯作者:
罗炜
E-mail:2237087676@qq.com
Gang LEI, Wei LUO(), Yunshu LI, Canhui LAI
Received:
2023-03-30
Revised:
2023-04-27
Accepted:
2023-05-16
Online:
2023-08-15
Published:
2023-05-18
Contact:
Wei LUO
E-mail:2237087676@qq.com
摘要:
针对高超声速滑翔飞行器航迹规划中面临的复杂环境约束问题,提出了一种结合几何-动力学的航路点跟踪方法并设计了一种禁飞区约束简化策略。首先,在通过飞行走廊确定飞行过程中航向角变化范围的基础上,以角度为指标设计代价函数,并基于此对飞行状态进行预测寻优,得到了倾侧角自适应搜索的横向机动模型;其次,将几何平面上的虚拟航路点生成策略拓展到地球曲面,并基于图论思想和动力学评估模型,获得了全局最佳虚拟航路点生成策略;最后,将2种方法结合得到解决多禁飞区约束的航迹规划方法。仿真结果表明,所提方法能够快速有效获得最佳虚拟航路点,并且降低航迹规划中的倾侧角优化难度;蒙特卡洛仿真实验表明,本方法具有较好的鲁棒性。
中图分类号:
雷刚, 罗炜, 李云舒, 赖灿辉. 高超声速滑翔飞行器多禁飞区再入机动航迹优化[J]. 航空学报, 2023, 44(15): 528769-528769.
Gang LEI, Wei LUO, Yunshu LI, Canhui LAI. Optimization of reentry maneuver trajectory for hypersonic glide vehicles in multiple no-fly zones[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528769-528769.
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