Guidance Laws Based on Optimal Feedback Linearization Pseudocontrol with Time-to-Go Estimation

Journal of Guidance, Control, and Dynamics - Tập 37 Số 4 - Trang 1298-1305 - 2014
David Alkaher1, Amiram Moshaiov1, Yizhar Or2
1The Iby and Aladar Fleischman Faculty of Engineering, Tel-Aviv University, 69978 Tel Aviv, Israel
2Faculty of Mechanical Engineering, Faculty of Mechanical Engineering, Technion—Israel Institute of Technology, 32000 Haifa, Israel

Tóm tắt

Từ khóa


Tài liệu tham khảo

10.1533/9781782420590.77

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Ben-Asher J., 1998, Advances in Missile Guidance Theory, 180, 25

10.1109/7.135432

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Thông tin xuất bản

Journal of Guidance, Control, and Dynamics

Tập 37 Số 4

1298-1305

Thông tin tác giả