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Điều Khiển Tư Thế Phối Hợp cho Vệ Tinh Radar Tổng Hợp với Tín Hiệu Lượng Tử và Độ Trễ Giao Tiếp
Tóm tắt
Bài báo này nghiên cứu vấn đề điều khiển tư thế phối hợp của các vệ tinh radar tổng hợp và đề xuất hai loại phương pháp điều khiển chế độ trượt cuối. Phương pháp điều khiển đầu tiên được nghiên cứu dựa trên cách tiếp cận chế độ trượt cuối không suy biến thông thường và các tham số Rodrigues đã được sửa đổi với sự xem xét đến việc lượng tử tín hiệu và độ trễ giao tiếp. Dựa trên phương pháp điều khiển đầu tiên, chúng tôi phát triển phương pháp điều khiển thứ hai với điều kiện kích hoạt sự kiện dựa trên tích phân nhằm giảm tần suất cập nhật lệnh điều khiển từ các bộ điều khiển tới các bộ truyền động. Cuối cùng, các ví dụ mô phỏng số dựa trên một cụm ba vệ tinh được trình bày để cho thấy tính hiệu quả của hai phương pháp điều khiển đã được thiết kế.
Từ khóa
#điều khiển tư thế #radar tổng hợp #lượng tử tín hiệu #độ trễ giao tiếp #chế độ trượt cuốiTài liệu tham khảo
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