Integrated Guidance and Control of Missiles with θ-D Method

IFAC Proceedings Volumes - Tập 37 Số 6 - Trang 629-634 - 2004
Ming Xin1, S.N. Balakrishnan1, Ernest Ohlmeyer2
1Department of Mechanical & Aerospace Engineering, University of Missouri-Rolla Rolla, MO 65401, USA
2Naval Surface Weapon Center, Dahlgren, VA 22448-5000, USA

Tóm tắt

Từ khóa


Tài liệu tham khảo

Bryson, 1975

Cloutier, 1999, Control of a Continuously Stirred Tank Reactor Using an Asymmetric Solution of the State-Dependent Riccati Equation, Proceedings of the IEEE Conference on Control Applications, Vol. 2, 893

Evers, 1992, Application of Integrated Guidance and Control Schemes to a Precision Guided Missile, Proceedings of American Control Conference, Vol. 3, 3225

Isidori, 1995

Lin, 1984, Optimal Controller for Homing Missiles, Proceedings of American Control Conference, Vol. 2, 737

Menon, 1996, Robust Nonlinear Control Technology for High-Agility Missile Interceptors, Optimal Synthesis,

Menon, 1999, Integrated Design of Agile Missile Guidance and Control Systems, Proceedings of the 7th Mediterranean Conference on Control and Automation, Vol. 3, 1469

Menon, 2001, Nonlinear Integrated Guidance and Control Laws For Homing Missiles

Xin, 2002, A New Method for Suboptimal Control of A Class of Nonlinear Systems

Zarchan, 1995, Proportional Navigation and Weaving Targets, Journal of Guidance, Control and Dynamics, Vol. 18, 10.2514/3.21492