Developed Time-Optimal Model Predictive Static Programming Method with Fish Swarm Optimization for Near-Space Vehicle

被引:0
作者
Wang, Yuanzhuo [1 ]
Dai, Honghua [1 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
来源
CMES-COMPUTER MODELING IN ENGINEERING & SCIENCES | 2025年
基金
美国国家科学基金会; 中国国家自然科学基金;
关键词
Near-space vehicle; model predictive static programming; neighboring term and trust region; optimal control; adaptive fish swarm optimization; TRAJECTORY OPTIMIZATION; MIDCOURSE GUIDANCE; CONTROLLER;
D O I
10.32604/cmes.2025.064416
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
To establish the optimal reference trajectory for a near-space vehicle under free terminal time, a timeoptimal model predictive static programming method is proposed with adaptive fish swarm optimization. First, the model predictive static programming method is developed by incorporating neighboring terms and trust region, enabling rapid generation of precise optimal solutions. Next, an adaptive fish swarm optimization technique is employed to identify a sub-optimal solution, while a momentum gradient descent method with learning rate decay ensures the convergence to the global optimal solution. To validate the feasibility and accuracy of the proposed method, a near-space vehicle example is analyzed and simulated during its glide phase. The simulation results demonstrate that the proposed method aligns with theoretical derivations and outperforms existing methods in terms of convergence speed and accuracy. Therefore, the proposed method offers significant practical value for solving the fast trajectory optimization problem in near-space vehicle applications.
引用
收藏
页码:1463 / 1484
页数:22
相关论文
共 42 条
[1]  
Antony T., 2018, dissertation's thesis
[2]   Survey of numerical methods for trajectory optimization [J].
Betts, JT .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1998, 21 (02) :193-207
[3]  
Bryson A.E., 1975, Applied Optimal Control: Optimization, Estimation, and Control, DOI [10.1109/TSMC.1979.4310229, DOI 10.1109/TSMC.1979.4310229]
[4]   A review of optimization techniques in spacecraft flight trajectory design [J].
Chai, Runqi ;
Savvaris, Al ;
Tsourdos, Antonios ;
Chai, Senchun ;
Xia, Yuanqing .
PROGRESS IN AEROSPACE SCIENCES, 2019, 109
[5]   Time-efficient approximate trajectory planning for AoI-centered multi-UAV IoT networks [J].
Chapnevis, Amirahmad ;
Bulut, Eyuphan .
INTERNET OF THINGS, 2025, 29
[6]   Optimal Trajectories of a UAV Base Station Using Hamilton-Jacobi Equations [J].
Coupechoux, Marceau ;
Darbon, Jerome ;
Kelif, Jean-Marc ;
Sigelle, Marc .
IEEE TRANSACTIONS ON MOBILE COMPUTING, 2023, 22 (08) :4837-4849
[7]   Novel Finite-Time Controller With Improved Auxiliary Adaptive Law for Hypersonic Vehicle Subject to Actuator Constraints [J].
Ding, Yibo ;
Yue, Xiaokui ;
Li, Wenbo ;
Huang, Panxing ;
Li, Naying .
IEEE TRANSACTIONS ON INTELLIGENT TRANSPORTATION SYSTEMS, 2025, 26 (03) :3402-3416
[8]   Review of control and guidance technology on hypersonic vehicle [J].
Ding, Yibo ;
Yue, Xiaokui ;
Chen, Guangshan ;
Si, Jiashun .
CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (07) :1-18
[9]   Finite-time controller design with adaptive fixed-time anti-saturation compensator for hypersonic vehicle [J].
Ding, Yibo ;
Yue, Xiaokui ;
Liu, Chuang ;
Dai, Honghua ;
Chen, Guangshan .
ISA TRANSACTIONS, 2022, 122 :96-113
[10]   Suboptimal Midcourse Guidance of Interceptors for High-Speed Targets with Alignment Angle Constraint [J].
Dwivedi, Prasiddha Nath ;
Bhattacharya, Abhijit ;
Padhi, Radhakant .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2011, 34 (03) :860-877