Time-to-go weighted optimal guidance with impact angle constraints

IEEE Transactions on Control Systems Technology - Tập 14 Số 3 - Trang 483-492 - 2006
Chang-Kyung Ryoo1, Hangju Cho1, Min-Jea Tahk2
1Agency for Defence Development, Daejeon, South Korea
2Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon, South Korea

Tóm tắt

Từ khóa


Tài liệu tham khảo

10.1109/7.640285

10.1016/S0967-0661(03)00097-2

felio, 2000, Lecture Note on Autonomous Vehicle Guidance Control and Simulation

lin, 1991, Modern Navigation Guidance and Control Processing, 360

10.2514/3.56061

10.2514/3.50527

10.2514/2.4585

khalil, 2002, Nonlinear System

10.1109/7.993225

zarchan, 1994, Tactical and Strategic Missile Guidance, 45

ben-asher, 1998, Advances in Missile Guidance Theory, 180, 25

cho, 1992, navigation constants in png law and the associated optimal control problems, Proc Kor Automatic Control Conf, 578

ryoo, 2003, closed-form solutions of optimal guidance with terminal impact angle constraint, Proc IEEE Int Conf Control Application, 504, 10.1109/CCA.2003.1223469

10.1109/7.805460

10.1109/ACC.2003.1238981

10.2514/1.8392

10.1109/TAES.1973.309659

bryson jr, 1975, Applied Optimal Control

10.2514/6.2003-5795