This work develops a frequency domain loop shaping design strategy based on linear quadratic gaussian controllers with loop transfer recovery (LQG/LTR). The design strategy presented is an integrated design synthesis procedure which is conducive to educated trade-off management. The controller design specification are expressed in terms of loop shaping bounds for load dynamic and model uncertainties, command response times and disturbance response times. The design philosophy is to first and foremost satisfy the stability constraints subject to the model variation specification and then to satisfy the time domain design specifications. The LQG/LTR controller is synthesised in discrete time, the resulting design is a Robust-Optimal design. A...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
Linear-Quadratic-Gaussian (LQG) control is a modern state-space technique for designing optimal dyna...
A set of guidance control laws is developed for application to a reduced order dynamic aircraft mode...
This work develops a frequency domain loop shaping design strategy based on linear quadratic gaussia...
The brushless servo drive is arguably the most important emerging drive category for robotics, machi...
A discussion of identification methods employed in process control applications is carried out. The ...
The automation of the operation of aircraft equipment lightens and diminishes the manipulation of th...
Designing electronic control systems specific to additive manufacturing machines is a fast evolving ...
This paper presents the development of Linear Quadratic Gaussian controller design forDC servo moto...
Dissertation (Ph.D.) University of Alaska Fairbanks, 2009We present applications of some methods of ...
This thesis deals with the Boyd-Barratt paradigm for feedback controller design. The Boyd-Barratt ap...
This work develops a new paradigm for optimal robust controller synthesis in the frequency domain. A...
Includes bibliographical references (p. 87-92).Supported by Wright Patterson Air Force Base. F33615-...
With the advancement of power electronic technologies over recent decades, there has been an overall...
In this dissertation we discuss loop-shaping algorithms that bring enhanced servo performance at mul...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
Linear-Quadratic-Gaussian (LQG) control is a modern state-space technique for designing optimal dyna...
A set of guidance control laws is developed for application to a reduced order dynamic aircraft mode...
This work develops a frequency domain loop shaping design strategy based on linear quadratic gaussia...
The brushless servo drive is arguably the most important emerging drive category for robotics, machi...
A discussion of identification methods employed in process control applications is carried out. The ...
The automation of the operation of aircraft equipment lightens and diminishes the manipulation of th...
Designing electronic control systems specific to additive manufacturing machines is a fast evolving ...
This paper presents the development of Linear Quadratic Gaussian controller design forDC servo moto...
Dissertation (Ph.D.) University of Alaska Fairbanks, 2009We present applications of some methods of ...
This thesis deals with the Boyd-Barratt paradigm for feedback controller design. The Boyd-Barratt ap...
This work develops a new paradigm for optimal robust controller synthesis in the frequency domain. A...
Includes bibliographical references (p. 87-92).Supported by Wright Patterson Air Force Base. F33615-...
With the advancement of power electronic technologies over recent decades, there has been an overall...
In this dissertation we discuss loop-shaping algorithms that bring enhanced servo performance at mul...
AbstractThis paper, describes a LQG and LQR robust controller for the lateral and longitudinal fligh...
Linear-Quadratic-Gaussian (LQG) control is a modern state-space technique for designing optimal dyna...
A set of guidance control laws is developed for application to a reduced order dynamic aircraft mode...