| dc.contributor |
Department of Mechanical and Aerospace Engineering |
|
| dc.creator |
Yoon, H. |
|
| dc.creator |
Agrawal, B.N. |
|
| dc.date |
2013-07-18T19:18:27Z |
|
| dc.date |
2013-07-18T19:18:27Z |
|
| dc.date |
2008 |
|
| dc.date.accessioned |
2022-05-19T00:35:11Z |
|
| dc.date.available |
2022-05-19T00:35:11Z |
|
| dc.identifier |
American Control Conference, Seattle, WA June 11-13, 2008. |
|
| dc.identifier |
http://hdl.handle.net/10945/34537 |
|
| dc.identifier.uri |
http://localhost:8080/xmlui/handle/CUHPOERS/58404 |
|
| dc.description |
The article of record as published may be found at http://dx.doi.org/10.1109/ACC.2008.4586947 |
|
| dc.description |
A novel adaptive tracking control law for nonlinear Hamiltonian multi-input–multi-output (MIMO) systems with uncertain parameters in the actuator modeling as well as the inertia and/or the Coriolis and centrifugal terms is developed. The physical properties of the Hamiltonian systems are effectively used in the control design and the stability analysis. The number of the parameter estimates is significantly lowered as compared to the conventional adaptive control methods which are based on the statespace form. The developed control scheme is applied for attitude control of a spacecraft with both the inertia and the actuator uncertainties, and numerical examples show that the controller successfully deals with the unknown inertia/actuator parameters. |
|
| dc.format |
application/pdf |
|
| dc.rights |
This publication is a work of the U.S. Government as defined
in Title 17, United States Code, Section 101. As such, it is in the
public domain, and under the provisions of Title 17, United States
Code, Section 105, is not copyrighted in the U.S. |
|
| dc.title |
Adaptive Control of Uncertain Hamiltonian Multi-Input Multi-Output Systems: with Application to Spacecraft Control |
|