Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure

Aerospace Science and Technology - Tập 53 - Trang 169-187 - 2016
Weihong Wang1,2, Shaofeng Xiong3,1,2, Sen Wang1,2, Siyang Song1,2, Chao Lai1,2
1School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China
2Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China
3Beijing Institute of Space Launch Technology, Beijing 100076, China

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Tài liệu tham khảo

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