Nonlinear longitudinal acceleration control of nonminimum phase missiles with actuator dynamics
暂无分享,去创建一个
[1] Min-Jea Tahk,et al. Plant Inversion Control of Tail-Controlled Missiles , 1997 .
[2] Jae-Hyuk Oh,et al. Missile autopilot design via functional inversion and time-scaled transformation , 1997 .
[3] Dongkyoung Chwa,et al. Multi-Input Multi-Output Nonlinear Autopilot Design for Ship-to-Ship Missiles , 2006 .
[4] Pramod P. Khargonekar,et al. Missile Autopilot Designs Using H8 Control with Gain Scheduling and Dynamic Inversion , 1998 .
[5] Byoung Soo Kim,et al. Pitch Autopilot Design for Agile Missiles with Uncertain Aerodynamic Coefficients , 2013, IEEE Transactions on Aerospace and Electronic Systems.
[6] Alexander Zhurbal,et al. Effect of Estimation on the Performance of an Integrated Missile Guidance and Control System , 2011, IEEE Transactions on Aerospace and Electronic Systems.
[7] Dongkyoung Chwa,et al. Compensation of actuator dynamics in nonlinear missile control , 2004, IEEE Transactions on Control Systems Technology.
[8] J.R. Cloutier,et al. Robust feedback linearization approach to autopilot design , 1992, [Proceedings 1992] The First IEEE Conference on Control Applications.
[9] Gene F. Franklin,et al. Feedback Control of Dynamic Systems , 1986 .
[10] Min-Jea Tahk,et al. Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint , 2012, IEEE Transactions on Aerospace and Electronic Systems.
[11] Dongkyoung Chwa,et al. New parametric affine modeling and control for skid-to-turn missiles , 2001, IEEE Trans. Control. Syst. Technol..
[12] Lei Guo,et al. Nonlinear-Disturbance-Observer-Based Robust Flight Control for Airbreathing Hypersonic Vehicles , 2013, IEEE Transactions on Aerospace and Electronic Systems.
[13] In-Joong Ha,et al. Autopilot design for highly maneuvering STT missiles via singular perturbation-like technique , 1999, IEEE Trans. Control. Syst. Technol..
[14] Zhihua Qu,et al. Design and evaluation of robust nonlinear missile autopilots from a performance perspective , 1995, Proceedings of 1995 American Control Conference - ACC'95.
[15] Jin Young Choi,et al. Adaptive control based on a parametric affine model for tail-controlled missiles , 2000, Proceedings of the 39th IEEE Conference on Decision and Control (Cat. No.00CH37187).
[16] Sreenatha G. Anavatti,et al. Observer-based adaptive guidance law considering target uncertainties and control loop dynamics , 2006, IEEE Transactions on Control Systems Technology.
[17] Min-Jea Tahk,et al. Time-to-go Polynomial Guidance with Trajectory Modulation for Observability Enhancement , 2013, IEEE Transactions on Aerospace and Electronic Systems.
[18] Min-Jea Tahk,et al. Optimality of Linear Time-Varying Guidance for Impact Angle Control , 2012, IEEE Transactions on Aerospace and Electronic Systems.
[19] Seon-Gab Kim,et al. Output-redefinition based on robust zero dynamics = 강인 제로 동역학에 기초한 출력재정의 기법 , 1998 .
[20] Swaroop Darbha,et al. Dynamic surface control for a class of nonlinear systems , 2000, IEEE Trans. Autom. Control..
[21] Hyo-Sang Shin,et al. Energy Optimal Waypoint Guidance Synthesis for Antiship Missiles , 2010, IEEE Transactions on Aerospace and Electronic Systems.
[22] Warren E. Dixon,et al. Lyapunov-Based Control of Robotic Systems , 2009 .
[23] Dongkyoung Chwa,et al. Adaptive nonlinear guidance law considering control loop dynamics , 2003 .
[24] Sanjay E. Talole,et al. Sliding Mode and Inertial Delay Control Based Missile Guidance , 2012, IEEE Transactions on Aerospace and Electronic Systems.
[25] Christopher D'Souza,et al. Missile flight control with dynamic inversion and structured singular value synthesis , 1994 .
[26] Abbas Emami-Naeini,et al. Feedback Control of Dynamic Systems (6th edition) , 2010 .
[27] A. Levant,et al. Guidance and Control of Missile Interceptor using Second-Order Sliding Modes , 2009, IEEE Transactions on Aerospace and Electronic Systems.
[28] Zhihua Qu,et al. Dynamic robust recursive control design and its application to a nonlinear missile autopilot , 1997, Proceedings of the 1997 American Control Conference (Cat. No.97CH36041).
[29] In-Joong Ha,et al. A learning approach to precision speed control of servomotors and its application to a VCR , 1999, IEEE Trans. Control. Syst. Technol..
[30] Jinho Kim,et al. Nonlinear model inversion control for bank-to-turn missile , 1995 .
[31] Chang-Hun Lee,et al. Polynomial Guidance Laws Considering Terminal Impact Angle and Acceleration Constraints , 2013, IEEE Transactions on Aerospace and Electronic Systems.