Fixed-time cooperative trajectory optimisation strategy for multiple hypersonic gliding vehicles based on neural network and ABC algorithm
被引:1
作者:
Zhang, X.
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机构:
Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R ChinaNorthwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Zhang, X.
[1
]
Liu, S.
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机构:
Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Shanghai Arospace Equipment Manufacturer Co Ltd, Shanghai 200245, Peoples R ChinaNorthwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Liu, S.
[1
,2
]
Yan, J.
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机构:
Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R ChinaNorthwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Yan, J.
[1
]
Liu, S.
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h-index: 0
机构:
Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Shanghai Arospace Equipment Manufacturer Co Ltd, Shanghai 200245, Peoples R ChinaNorthwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Liu, S.
[1
,2
]
Yan, B.
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机构:
Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R ChinaNorthwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
Yan, B.
[3
]
机构:
[1] Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
[2] Shanghai Arospace Equipment Manufacturer Co Ltd, Shanghai 200245, Peoples R China
[3] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
Collaborative planning for multiple hypersonic vehicles can effectively improve operational effectiveness. Time coordination is one of the main forms of cooperation among multi-hypersonic glide vehicles, and time cooperation trajectory optimisation is a key technology that can significantly increase the success rate of flight missions. However, it is difficult to obtain satisfactory time as a constraint condition during trajectory optimisation. To solve this problem, a multilayer Perceptrona is trained and adopted in a time-decision module, whose input is a four-dimensional vector selected according to the trajectory characteristics. Additionally, the MLP will be capable of determining the optimal initial heading angle of each aircraft to reduce unnecessary manoeuvering performance consumption in the flight mission. Subsequently, to improve the cooperative flight performance of hypersonic glide vehicles, the speed-dependent angle-of-attack and bank command were designed and optimised using the Artificial Bee Colony algorithm. The final simulation results show that the novel strategy proposed in this study can satisfy terminal space constraints and collaborative time constraints simultaneously. Meanwhile, each aircraft saves an average of 13.08% flight range, and the terminal speed is increased by 315.6m/s compared to the optimisation results of general purpose optimal control software (GPOPS) tools.
机构:
Harbin Inst Technol, Ctr Control Theory & Guidance Technol, 92 West Dazhi St, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Ctr Control Theory & Guidance Technol, 92 West Dazhi St, Harbin 150001, Peoples R China
Li, Jianfeng
Song, Shenmin
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Harbin Inst Technol, Ctr Control Theory & Guidance Technol, 92 West Dazhi St, Harbin 150001, Peoples R ChinaHarbin Inst Technol, Ctr Control Theory & Guidance Technol, 92 West Dazhi St, Harbin 150001, Peoples R China
Song, Shenmin
Shi, Xiaoping
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Harbin Inst Technol, Control & Simulat Ctr, Harbin, Peoples R ChinaHarbin Inst Technol, Ctr Control Theory & Guidance Technol, 92 West Dazhi St, Harbin 150001, Peoples R China
机构:
Sun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R ChinaSun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R China
Lu, Xinyue
Wang, Jianying
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机构:
Sun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R ChinaSun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R China
Wang, Jianying
Wang, Yonghai
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机构:
China Acad Launch Vehicle Technol, Beijing 100076, Peoples R ChinaSun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R China
Wang, Yonghai
Chen, Jun
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机构:
China Acad Launch Vehicle Technol, Beijing 100076, Peoples R ChinaSun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R China
机构:
Nanjing Univ Sci & Technol, Sch Automat, Sino French Int Joint Lab Automat Control & Signal, Nanjing 210094, Peoples R ChinaNanjing Univ Sci & Technol, Sch Automat, Sino French Int Joint Lab Automat Control & Signal, Nanjing 210094, Peoples R China
Zhou, Xingyu
Wang, Haoping
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机构:
Nanjing Univ Sci & Technol, Sch Automat, Sino French Int Joint Lab Automat Control & Signal, Nanjing 210094, Peoples R ChinaNanjing Univ Sci & Technol, Sch Automat, Sino French Int Joint Lab Automat Control & Signal, Nanjing 210094, Peoples R China
Wang, Haoping
Wu, Ke
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机构:
INRIA Lille Nord Europe, 40 Ave Halley, Lille F-59000, FranceNanjing Univ Sci & Technol, Sch Automat, Sino French Int Joint Lab Automat Control & Signal, Nanjing 210094, Peoples R China
Wu, Ke
Zheng, Gang
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机构:
INRIA Lille Nord Europe, 40 Ave Halley, Lille F-59000, FranceNanjing Univ Sci & Technol, Sch Automat, Sino French Int Joint Lab Automat Control & Signal, Nanjing 210094, Peoples R China