A New Midcourse Guidance Design for Near Space Target Interceptor

This study proposes a new midcourse guidance method, combining the trajectory optimization approach and the optimal sliding mode method, to decrease the larger relative velocity between the near space target and the interceptor. Firstly, the midcourse trajectory optimization model is established. Th...

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Vydáno v:IEEE access Ročník 8; s. 17642 - 17651
Hlavní autoři: Wu, Yanrui, Xiao, Mingqing, Zhang, Danxu, Peng, Weishi, Xu, Yang, Dong, Xinyu
Médium: Journal Article
Jazyk:angličtina
Vydáno: Piscataway IEEE 2020
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Témata:
Aerodynamics
Aerospace electronics
Guidance (motion)
Hafnium
Heating systems
Maneuverability
Mathematical models
Midcourse guidance
Midcourse trajectories
Near space target interceptor
Optimal control
optimal sliding mode control
Optimization
Sliding mode control
three-dimensional midcourse guidance
Trajectory optimization
trajectory optimization online
ISSN:2169-3536, 2169-3536
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Shrnutí:This study proposes a new midcourse guidance method, combining the trajectory optimization approach and the optimal sliding mode method, to decrease the larger relative velocity between the near space target and the interceptor. Firstly, the midcourse trajectory optimization model is established. Then, the trajectory optimization guidance law based on a sampling scheme is proposed to decrease the larger relative velocity and satisfy multiple constraints at the end time of the midcourse guidance phase. Thirdly, the optimal sliding mode guidance law is introduced to deal with the target maneuverability. Finally, numerical simulations were performed to verify the performance of the midcourse guidance law.
Bibliografie:ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 14
ISSN:2169-3536
2169-3536
DOI:10.1109/ACCESS.2020.2966248