A new sliding mode control design for integrated missile guidance and control system

Aerospace Science and Technology - Tập 78 - Trang 54-61 - 2018
Jianguo Guo1, Yu Xiong1, Jun Zhou1
1Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi'an 710072, China

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Tài liệu tham khảo

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