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变构型多操纵面RLV进场着陆轨迹优化设计

郝现伟 王勇 杨业 郭涛

郝现伟, 王勇, 杨业, 等 . 变构型多操纵面RLV进场着陆轨迹优化设计[J]. 北京航空航天大学学报, 2015, 41(12): 2232-2239. doi: 10.13700/j.bh.1001-5965.2014.0822
引用本文: 郝现伟, 王勇, 杨业, 等 . 变构型多操纵面RLV进场着陆轨迹优化设计[J]. 北京航空航天大学学报, 2015, 41(12): 2232-2239. doi: 10.13700/j.bh.1001-5965.2014.0822
HAO Xianwei, WANG Yong, YANG Ye, et al. Optimization design of approach and landing trajectory for variable configuration RLV with multi-control surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(12): 2232-2239. doi: 10.13700/j.bh.1001-5965.2014.0822(in Chinese)
Citation: HAO Xianwei, WANG Yong, YANG Ye, et al. Optimization design of approach and landing trajectory for variable configuration RLV with multi-control surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(12): 2232-2239. doi: 10.13700/j.bh.1001-5965.2014.0822(in Chinese)

变构型多操纵面RLV进场着陆轨迹优化设计

doi: 10.13700/j.bh.1001-5965.2014.0822
基金项目: 总装预研重点项目(9140A25030109HK0103)
详细信息
    作者简介:

    郝现伟(1985-),男,山东聊城人,博士研究生,haoxw_1220@163.com

    通讯作者:

    王勇(1966-),男,湖北襄阳人,研究员,wy_buaa@sina.com,主要研究方向为无人驾驶飞行器飞行控制.

  • 中图分类号: V417+.6;V249.32

Optimization design of approach and landing trajectory for variable configuration RLV with multi-control surfaces

  • 摘要: 针对变构型多操纵面可重复使用飞行器(RLV)的进场着陆问题,提出了一种进场着陆轨迹设计方法.将进场着陆轨迹分为深下滑着陆轨迹和拉平着陆轨迹;考虑了气动舵面可操纵偏转限制及深下滑拟平衡约束条件,对深下滑着陆轨迹进行了优化设计;考虑了RLV气动舵面调节余量和构型变化过程,以起落架放下时间、拉平法向过载及接地状态为约束,基于RLV动力学方程,采用轨迹推演的方法对拉平着陆轨迹进行了优化设计.深下滑着陆轨迹和拉平着陆轨迹组成完整的进场着陆轨迹,所设计的着陆轨迹综合考虑了多种约束条件,提高了着陆过程平稳性和安全性.

     

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出版历程
  • 收稿日期:  2014-12-29
  • 修回日期:  2015-04-03
  • 网络出版日期:  2015-12-20

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