Integrated guidance and control with input saturation and disturbance observer

In presence of input saturation, a novel integrated guidance and control (IGC) law based on the backstepping technique is proposed for missiles attacking manoeuvring target in this paper. A modifie...

[1]  Xiao-Geng Liang,et al.  Integrated guidance and control based on block backstepping sliding mode and dynamic control allocation , 2015 .

[2]  Mou Chen,et al.  Terminal sliding mode tracking control for a class of SISO uncertain nonlinear systems. , 2013, ISA transactions.

[3]  Gang Tao,et al.  A novel nonlinear resilient control for a quadrotor UAV via backstepping control and nonlinear disturbance observer , 2016 .

[4]  Beibei Ren,et al.  Anti-disturbance control of hypersonic flight vehicles with input saturation using disturbance observer , 2015, Science China Information Sciences.

[5]  Duan Guangren,et al.  Integrated guidance and control for missile in the presence of input saturation and angular constraints , 2013, Proceedings of the 32nd Chinese Control Conference.

[6]  Liu Gang,et al.  Integrated Guidance and Control Design for the Near Space Interceptor , 2015 .

[7]  E. J. Ohlmeyer,et al.  Numerical State-Dependent Riccati Equation Approach for Missile Integrated Guidance Control , 2009 .

[8]  Gang Tao,et al.  Robust Backstepping Sliding-Mode Control and Observer-Based Fault Estimation for a Quadrotor UAV , 2016, IEEE Transactions on Industrial Electronics.

[9]  Yuri B. Shtessel,et al.  Integrated Higher-Order Sliding Mode Guidance and Autopilot for Dual Control Missiles , 2009 .

[10]  Xianghua Wang,et al.  Partial Integrated Guidance and Control with Impact Angle Constraints , 2015 .

[11]  Guangren Duan,et al.  Adaptive Dynamic Surface Control for Integrated Missile Guidance and Autopilot in the Presence of Input Saturation , 2015 .

[12]  Dong Xu,et al.  Missile Guidance Law Based on Extended State Observer , 2013, IEEE Transactions on Industrial Electronics.

[13]  Jie Wu,et al.  Integrated guidance and control with L 2 disturbance attenuation for hypersonic vehicles , 2016 .

[14]  Gang Tao,et al.  Direct self-repairing control for a helicopter via quantum multi-model and disturbance observer , 2016, Int. J. Syst. Sci..

[15]  Bernard Friedland,et al.  Design of an integrated strapdown guidance and control system for a tactical missile , 1983 .

[16]  D. S. Malyevac,et al.  Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads , 2004 .

[17]  Sen Wang,et al.  Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure , 2016 .

[18]  Bin Fu,et al.  Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach , 2015 .

[19]  Di Zhou,et al.  Adaptive Dynamic Surface Guidance Law with Input Saturation Constraint and Autopilot Dynamics , 2016 .

[20]  Lifei Chen.  A probabilistic framework for optimizing projected clusters with categorical attributes , 2014, Science China Information Sciences.

[21]  Xinghuo Yu,et al.  Terminal sliding mode control of MIMO linear systems , 1997 .

[22]  Mohammad Haeri,et al.  Integrated guidance and control of elastic flight vehicle based on robust MPC , 2015 .

[23]  E. J. Ohlmeyer,et al.  Integrated Design of Agile Missile Guidance and Autopilot Systems , 2001 .

[24]  Qun Zong,et al.  Integrated guidance and control for reusable launch vehicle in reentry phase , 2015 .

[25]  Qing Wang,et al.  Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control , 2014 .

[26]  Yongduan Song,et al.  Design of a Unified Power Controller for Variable-Speed Fixed-Pitch Wind Energy Conversion System , 2016, IEEE Transactions on Industrial Electronics.

[27]  Tao Zhang,et al.  L 1 adaptive state feedback controller for three-dimensional integrated guidance and control of interceptor , 2014 .

[28]  Guangren Duan,et al.  Adaptive block dynamic surface control for integrated missile guidance and autopilot , 2013 .

[29]  Jinzhi Wang,et al.  Partial Integrated Guidance and Control for Missiles with Three-Dimensional Impact Angle Constraints , 2014 .

[30]  Ernest J. Ohlmeyer,et al.  Optimal Design of Integrated Missile Guidance and Control , 1998 .

[31]  Wang Honglun,et al.  Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO. , 2015, ISA transactions.

[32]  Tao Zhang,et al.  Integrated interceptor guidance and control with prescribed performance , 2015 .

[33]  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.

[34]  Haibo Ji,et al.  Integrated guidance and control for dual-control missiles based on small-gain theorem , 2012, Autom..

[35]  Jing Zhou,et al.  Robust Adaptive Control of Uncertain Nonlinear Systems in the Presence of Input Saturation and External Disturbance , 2011, IEEE Transactions on Automatic Control.