机构:
Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R ChinaBeijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
He, Shaoming
[1
]
Zhang, Xueyan
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机构:
Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
China Dev Bank, 16 Taipingqiao St, Beijing 100034, Peoples R ChinaBeijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
Zhang, Xueyan
[1
,2
]
Lin, Defu
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h-index: 0
机构:
Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R ChinaBeijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
Lin, Defu
[1
]
Lee, Chang-Hun
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机构:
Korea Adv Inst Sci & Technol, Dept Aerosp Engn, Daejeon 34141, South KoreaBeijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
Lee, Chang-Hun
[3
]
机构:
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] China Dev Bank, 16 Taipingqiao St, Beijing 100034, Peoples R China
[3] Korea Adv Inst Sci & Technol, Dept Aerosp Engn, Daejeon 34141, South Korea
Missile Guidance;
Maneuvering Target;
PI Guidance;
Adaptive Guidance;
ROBUSTNESS;
D O I:
10.1109/CCDC52312.2021.9602291
中图分类号:
TP [自动化技术、计算机技术];
学科分类号:
0812 ;
摘要:
This paper proposes a new proportional-Integral (PI) guidance law for maneuvering targets interception. We first investigate the physical interpretation of the PI guidance law and the analysis results reveal that the PI guidance law is exactly the same as a direct model reference adaptive guidance law: the integral term in PI control plays the same role as the adaptive law in adaptive control. Based on this fact, we suggest a new PI guidance law by leveraging a modified reference model to improve the transient performance. Numerical simulation results are conducted to validate the analytic findings.