首页 >

基于同伦解析递推的高超声速滑翔轨迹快速优化方法(航天运输系统自主制导与控制技术专栏)

张延坤1,韦常柱2,刘哲1   

  1. 1. 哈尔滨工业大学航天学院
    2. 哈尔滨工业大学航天工程系
  • 收稿日期:2026-03-04 修回日期:2026-04-22 出版日期:2026-04-27 发布日期:2026-04-27
  • 通讯作者: 刘哲
  • 基金资助:
    国家自然科学基金

Efficient Trajectory Optimization for Hypersonic Glide Vehicles Based on Homotopy Analytical Propagation

Yan-Kun ZHANG 2,Zhe LIU2   

  • Received:2026-03-04 Revised:2026-04-22 Online:2026-04-27 Published:2026-04-27
  • Contact: Zhe LIU
  • Supported by:
    National Natural Science Foundation of China

摘要: 针对高超声速滑翔飞行器再入轨迹优化面临的强非线性、多约束及高实时性要求等难题,提出了一种基于同伦解析递推的高效轨迹优化方法。首先,给出基于线性化动力学算子的同伦分析法,通过构造包含系统雅可比矩阵信息的辅助线性算子,推导出了状态变量的显式解析递推模型,实现了对飞行轨迹的高精度快速预测。其次,基于该解析解的显式结构,提出了一种半解析梯度计算策略,利用解析预测器的快速性,通过链式法则与前向灵敏度递推相结合的方式获取梯度信息,避免了传统数值积分求解变分方程的繁琐过程,在保证梯度精度的同时显著降低了计算负担。最后,构建了基于原对偶内点法的轨迹优化框架,利用上述高效梯度信息引导搜索,在保证算法收敛性的同时,有效处理了热流、过载等高度非线性的过程与终端约束。仿真结果表明,所提出的解析递推算法在保证预测精度的同时,单次轨迹递推耗时仅为毫秒级;相比于传统伪谱法或数值打靶法,本文方法在计算速度上显著提升,能够生成严格满足所有飞行约束的平滑轨迹,具有在线应用的潜力。

关键词: 高超声速滑翔, 快速轨迹优化, 同伦分析法, 半解析灵敏度, 原对偶内点法

Abstract: To address the challenges of strong nonlinearity, multiple constraints, and stringent real-time requirements in the reentry trajectory optimization of Hypersonic Glide Vehicles (HGVs), an efficient trajectory optimization method based on Homotopy Analytical Propagation (HAP) is proposed. First, a homotopy analysis method based on a linearized dynamics operator is introduced. By constructing an auxiliary linear operator that incorporates the system Jacobian matrix, a set of explicit analytical recursive formulas for state variables is derived, achieving high-precision and rapid prediction of flight trajectories. Second, leveraging the explicit structure of the analytical solution, a semi-analytical gradient computation strategy is proposed. This strategy utilizes the computational efficiency of the analytical predictor to acquire gradient information through a combination of the chain rule and forward sensitivity propagation. This approach avoids the cumbersome numerical integration of variational equations, thereby significantly reducing the computational burden while maintaining gradient accuracy. Finally, a trajectory optimization framework based on the Primal-Dual Interior Point Method is established. By utilizing the aforementioned efficient gradient information to guide the search, this framework effectively handles highly nonlinear path and terminal constraints—such as heat flux and load factor—while ensuring algorithmic convergence. Simulation results demonstrate that the proposed analytical propagation algorithm achieves millisecond-level computational time for a single trajectory prediction while maintaining high accuracy. Compared with traditional pseudospectral methods or numerical shooting methods, the proposed method significantly improves computational speed and generates smooth trajectories that strictly satisfy all flight constraints, demonstrating significant potential for online applications.

Key words: Hypersonic Gliding, Efficient Trajectory Optimization, Homotopy Analysis Method, Semi-analytical Sensitivity, Interior Point Method

中图分类号: