Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft (Q647768)
From MaRDI portal
 | This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft |
scientific article; zbMATH DE number 5978752
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft |
scientific article; zbMATH DE number 5978752 |
Statements
Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft (English)
0 references
24 November 2011
0 references
robust output stabilization
0 references
nonlinear system
0 references
invariant ellipsoids
0 references
optimization problem
0 references
linear matrix inequalities
0 references
linear feedback
0 references
0 references
0 references
