“Compound Control Methodology for Flight Vehicles” focuses on new control methods for flight vehicles. In this monograph the concept of compound control is introduced. It is demonstrated that both Sliding Mode Control (SMC) and Active Disturbance Rejection Control (ADRC) have their own advantages and limitations, i.e., chattering of SMC and the observability of extended state observer (ESO), respectively. It is shown that compound control combines their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle ...
An overview of the active disturbance rejection control (ADRC) is presented in this talk. Ever since...
Automatic control is increasingly used in mission critical applications. The reason for this is the ...
The objective of the present dissertation is to show how redundant control surfaces can be exploited...
A compound control based on active disturbance rejection control (ADRC) scheme and slide mode contro...
An investigation into the application of an observer based sliding mode controller for robust contro...
The sliding mode control methodology has proven effective in dealing with complex dynamical systems ...
Active Disturbance Rejection Control (ADRC) offers a viable framework for flight control that both i...
The compound unmanned aircraft is provided with three primary flight modes, which are helicopter fli...
This book describes the advances and applications in Sliding mode control (SMC) which is widely used...
Sliding mode control is applied to the design of a flight control system capable of operating with l...
A brief review of sliding model control is undertaken, with particular emphasis upon the effects of ...
This thesis describes the development of robust discrete time sliding mode controllers where only ou...
Nonlinear Dynamic Inversion (NDI) is a promising method for Fault Tolerant Flight Control. The NDI a...
Sliding-mode control is one of the well-recognized non-linear control methods for nonlinear systems....
Sliding mode control (SMC) is a powerful and robust control method. SMC methods have been widely stu...
An overview of the active disturbance rejection control (ADRC) is presented in this talk. Ever since...
Automatic control is increasingly used in mission critical applications. The reason for this is the ...
The objective of the present dissertation is to show how redundant control surfaces can be exploited...
A compound control based on active disturbance rejection control (ADRC) scheme and slide mode contro...
An investigation into the application of an observer based sliding mode controller for robust contro...
The sliding mode control methodology has proven effective in dealing with complex dynamical systems ...
Active Disturbance Rejection Control (ADRC) offers a viable framework for flight control that both i...
The compound unmanned aircraft is provided with three primary flight modes, which are helicopter fli...
This book describes the advances and applications in Sliding mode control (SMC) which is widely used...
Sliding mode control is applied to the design of a flight control system capable of operating with l...
A brief review of sliding model control is undertaken, with particular emphasis upon the effects of ...
This thesis describes the development of robust discrete time sliding mode controllers where only ou...
Nonlinear Dynamic Inversion (NDI) is a promising method for Fault Tolerant Flight Control. The NDI a...
Sliding-mode control is one of the well-recognized non-linear control methods for nonlinear systems....
Sliding mode control (SMC) is a powerful and robust control method. SMC methods have been widely stu...
An overview of the active disturbance rejection control (ADRC) is presented in this talk. Ever since...
Automatic control is increasingly used in mission critical applications. The reason for this is the ...
The objective of the present dissertation is to show how redundant control surfaces can be exploited...