系统工程与电子技术 ›› 2026, Vol. 48 ›› Issue (4): 1331-1339.doi: 10.12305/j.issn.1001-506X.2026.04.21

• 系统工程 • 上一篇    

基于CUDA纹理插值的空间多目标交会序列 快速规划方法

刘浩(), 贺子鹏, 徐广德   

  1. 北京空间飞行器总体设计部,北京 100094
  • 收稿日期:2024-12-04 修回日期:2025-02-06 出版日期:2025-05-20 发布日期:2025-05-20
  • 通讯作者: 刘浩 E-mail:liuh188@qq.com
  • 作者简介:贺子鹏(1996—),男,工程师,硕士,主要研究方向为航天器系统工程以及任务规划
    徐广德(1990—),男,高级工程师,博士,主要研究方向为航天器总体设计

Fast planning method for space multi-target rendezvous sequence based on CUDA texture interpolation

Hao LIU(), Zipeng HE, Guangde XU   

  1. Beijing Institute of Spacecraft System Engineering,Beijing 100094,China
  • Received:2024-12-04 Revised:2025-02-06 Online:2025-05-20 Published:2025-05-20
  • Contact: Hao LIU E-mail:liuh188@qq.com

摘要:

针对卫星对多个异面目标连续交会的序列规划问题,提出基于计算统一设备架构(compute unified device architecture, CUDA)并行计算的快速规划方法。该方法以目标穿越卫星轨道面时刻为交会时机,首先形成交会候选方案集合,将目标间转移速度增量计算简化为基于转移速度和飞行角的双线性插值问题;然后利用纹理内存硬件插值快速估算速度增量,通过多线程块实现候选方案层面的并行化,并在单个候选方案内部通过并行规约和共享内存实现目标间转移速度增量计算的并行化以及总速度增量累加;最终对方案遍历寻优,实现速度增量最小化的多目标交会序列规划。仿真结果表明,此方法能够快速规划最优交会序列,相比串行计算可加速20倍以上,在智能算力逐步向太空普及的趋势下,未来可大幅提升多目标观测等场景的在轨规划效率。

关键词: 任务规划, 多目标序列规划, 并行计算, 计算统一设备架构

Abstract:

Aiming at the satellite sequence planning problem of continuous rendezvous with multiple noncoplanar targets, a fast planning method based on compute unified device architecture (CUDA) is proposed. The rendezvous timing is taken as the moment when the target crosses the orbital plane of the satellite. First, a set of candidate solutions for the rendezvous sequence is formed, and the calculation of the transfer velocity increment between targets based on the orbital dynamics model is simplified to a bilinear interpolation problem based on the transfer velocity and the flight angle. Then, texture memory is applied for fast estimation of the velocity increment, the parallelization at the level of candidate plan is realized by multiple thread blocks, and the parallelization of the transfer velocity increment calculation between targets and the accumulation of the total velocity increment are realized by parallel reduction and shared memory within a single candidate plan. Finally, an exhaustive search optimization approach is applied to the candidate solutions and the multi-target rendezvous sequence planning for minimizing the velocity increment is achieved. Simulation results show that this method can quickly plan the optimal rendezvous sequence, which is more than 20 times faster than serial calculation. As intelligent computing power gradually becomes more widespread in space, it is expected to significantly improve the efficiency of on-orbit planning for scenarios such as multi-target observation in the future.

Key words: mission planning, multiple-target sequence planning, parallel computing, compute unified device architecture (CUDA)

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