Shrinkage Estimation for a Dynamic Input-Output Linear Model

Author(s):  
Young-Won Kim ◽  
David M. Nickerson ◽  
I.V. Basawa
2021 ◽  
Vol 2131 (3) ◽  
pp. 032021
Author(s):  
A Voevoda ◽  
V Shipagin ◽  
K Bobobekov

Abstract Modification of the algorithm for the polynomial synthesis of a multi-channel controller was proposed to preserve all control channels in this article. In order to test the functionality of the proposed modification, an example of a linear model of an unstable multi-channel plant is considered. The choice of the plant was determined by the possibility of a visual algorithm demonstration for polynomial synthesis of the controller, taking into account the proposed modifications.The plant was represented as three series-connected standard links: an aperiodic link of the first order, an unstable link, and an integrator, and has three input and two output channels. The control in the system is carried out in the feedback of the system and is summed up with the input impact. The feature of the plant is to limit the task to the second output, since it is essentially a derivative of the first output. In addition, the plant has a direct input–output channel. That is, the traversal matrix of the system is nonzero (when described through the state space). The synthesis task was set as follows: it is necessary to achieve certain quality indicators of the output vector value while maintaining all three control channels of the plant.


2016 ◽  
Vol 8 (2) ◽  
pp. 160 ◽  
Author(s):  
Wenlan Ke ◽  
Jinghua Sha ◽  
Jingjing Yan ◽  
Guofeng Zhang ◽  
Rongrong Wu

Author(s):  
L Bruyere ◽  
A Tsourdos ◽  
B A White

An augmented lateral acceleration autopilot is designed for a model of a tactical missile and robust stability of the closed-loop system investigated. The tail-controlled missile in the cruciform fin configuration is modelled as a second-order quasi-linear parameter-varying system. This non-linear model is obtained from the Taylor linearized model of the horizontal motion by including explicit dependence of the aerodynamic derivatives on a state (side-slip velocity) and external parameters (longitudinal velocity and roll angle). The autopilot design is based on input-output pseudolinearization, which is a restriction of input-output feedback linearization to the set of equilibria of the non-linear model. The design makes Taylor linearization of the closed-loop system independent of the choice of equilibria. Thus, if the operating points are in the vicinity of the equilibria, then only one linear model will describe closed-loop dynamics, regardless of the rate of change in the operating points. Simulations for constant lateral acceleration demands show good tracking with fast response time. Robust autopilot design taking into account parametric stability margins for uncertainty aerodynamic derivatives is implemented using convex optimization and linear matrix inequalities.


2016 ◽  
Vol 103 ◽  
pp. 384-400 ◽  
Author(s):  
Lele Huang ◽  
Junlong Zhao ◽  
Huiwen Wang ◽  
Siyang Wang

1981 ◽  
Vol 103 (4) ◽  
pp. 370-374
Author(s):  
R. S. Baheti ◽  
R. R. Mohler

A dynamic model is developed to control the temperature of a specimen in a laboratory furnace. The control variables are the power input to the furnace and the rate of airflow inside the chamber. For a constant airflow input, the furnace can be represented by a linear model and a static gain dependent on the sample temperature. The power input to the furnace is perturbed with a pseudorandom binary sequence and the model parameters are estimated from the input-output measurements. The controller parameters are selected to minimize the variance in the sample temperature.


Author(s):  
Robert E. Skelton ◽  
Guojun Shi

Abstract An identifiability result determines whether there exists a linear time invariant model capable of matching the input/output data observed from experiments. If no match is possible, a method is presented to find the closest linear model to the data. A weighted q-Markov COVER method is introduced for identification.


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