TY - GEN
T1 - A new model reference control architecture for uncertain dynamical systems
AU - De La Torre, Gerardo
AU - Yucelen, Tansel
AU - Johnson, Eric
PY - 2012
Y1 - 2012
N2 - Here, a model reference control design is applied to uncertain dynamical systems. The design approach and related theory is inspired by both robust control and previous work in model reference adaptive control. The result is a simple (non-adaptive) control system with important performance guarantees against a general and uncertain dynamics. Similar to the design of adaptive controllers, we assume the existence of a parameterization of the system uncertainty. It is shown by using a recently proposed command governor architecture that if a priori knowledge of a conservative upper bound on the unknown ideal weight matrix is available, then it is possible not only to stabilize the uncertain dynamical system but also to achieve a guaranteed performance. Specifically, we show the controlled uncertain dynamical system approximates a given ideal reference system by properly choosing the design parameter of a command governor. Numerical examples illustrate the effectiveness of the proposed methodology.
AB - Here, a model reference control design is applied to uncertain dynamical systems. The design approach and related theory is inspired by both robust control and previous work in model reference adaptive control. The result is a simple (non-adaptive) control system with important performance guarantees against a general and uncertain dynamics. Similar to the design of adaptive controllers, we assume the existence of a parameterization of the system uncertainty. It is shown by using a recently proposed command governor architecture that if a priori knowledge of a conservative upper bound on the unknown ideal weight matrix is available, then it is possible not only to stabilize the uncertain dynamical system but also to achieve a guaranteed performance. Specifically, we show the controlled uncertain dynamical system approximates a given ideal reference system by properly choosing the design parameter of a command governor. Numerical examples illustrate the effectiveness of the proposed methodology.
UR - http://www.scopus.com/inward/record.url?scp=85087534675&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85087534675&partnerID=8YFLogxK
U2 - 10.2514/6.2012-5039
DO - 10.2514/6.2012-5039
M3 - Conference contribution
AN - SCOPUS:85087534675
SN - 9781600869389
T3 - AIAA Guidance, Navigation, and Control Conference 2012
BT - AIAA Guidance, Navigation, and Control Conference 2012
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA Guidance, Navigation, and Control Conference 2012
Y2 - 13 August 2012 through 16 August 2012
ER -