Kiểm soát ổn định tư thế vững chắc trong thời gian hữu hạn cho spacecraft cứng dưới ràng buộc vận tốc góc dựa trên mạng nơ-ron

Neural Computing and Applications - Tập 34 - Trang 5107-5117 - 2021
Bo Yu1, Haibo Du1,2, Lijian Ding1, Di Wu3, Hua Li1
1School of Electrical Engineering and Automation, Hefei University of Technology, Hefei, People’s Republic of China
2Engineering Technology search Center of Industrial Automation, Hefei, People’s Republic of China
3School of Automation, Southeast University, Nanjing, People’s Republic of China

Tóm tắt

Trong bài báo này, vấn đề kiểm soát ổn định tư thế của spacecraft trong điều kiện ràng buộc vận tốc góc được nghiên cứu. Một kế hoạch kiểm soát tư thế trong thời gian hữu hạn tuân theo ràng buộc trạng thái được thiết kế bằng cách tận dụng triệt để đặc điểm mô hình của quaternion. Dựa trên phương pháp chi phối đồng nhất, tính ổn định trong thời gian hữu hạn của hệ thống vòng kín được chứng minh. Nghiên cứu chứng minh rằng vận tốc góc có thể được giữ trong khoảng giới hạn vào bất kỳ thời điểm nào. Đối với hệ thống con động lực học vòng tư thế có nhiễu bên ngoài, một bộ điều khiển trượt tận cùng tích phân dựa trên mạng nơ-ron cơ sở bán kính được đề xuất. Cuối cùng, tính hợp lệ và những ưu điểm của kế hoạch điều khiển được đề xuất được chứng minh qua phần mô phỏng so với hai phương pháp điều khiển khác.

Từ khóa

#kiểm soát tư thế #mạng nơ-ron #vận tốc góc #ổn định #thời gian hữu hạn

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