An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system (Q811228)
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: An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system |
scientific article; zbMATH DE number 4215531
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system |
scientific article; zbMATH DE number 4215531 |
Statements
An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system (English)
0 references
1991
0 references
Dynamic modelling of various aerolastic control systems (e.g., an airfoil) requires an application of Söhngen's inversion formula for finite Hilbert transforms. In order to justify the validity of the inversion formula it is shown that the circulation history must belong to a weighted \(L_ 2\) space.
0 references
Dynamic modelling
0 references
aerolastic control systems
0 references
airfoil
0 references
Söhngen's inversion formula
0 references
Hilbert transforms
0 references
circulation
0 references
