Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method

Item

Title
Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method
Date
1965
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AFFDL TR 65-145 p. 72-83
Corporate Author
IBM San Jose Research Laboratory
Laboratory
Air Force Flight Dynamics Laboratory
Date Issued
1965-11-01
Extent
12
Identifier
AD0627048
Distribution Classification
1
Contract
AF 33(657)-11545
DoD Project
8225
DoD Task
822501
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Report Availability
Full text available
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
AFRL/VACA
Type
article
Format
1 online resource
Creator
Wang, P. K. C.

Linked resources

Items with "Has Part: Stability Analysis of a Simplified Pitch-Controlled Flexible Aerodynamic Vehicle Via Lyapunov's Direct Method"
Title Class
Papers on the Control of Distributed Aeroelastic Systems