Analytical Study Of Approximate Longitudinal Transfer Functions For A Flexible Airframe

Item

Title
Analytical Study Of Approximate Longitudinal Transfer Functions For A Flexible Airframe
Date
1962
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
ASD TDR 62-279
Creator
Pearce, B. F.
Johnson, W. A.
Siskind, R. K.
Corporate Author
Systems Technology Inc Inglewood Calif
Laboratory
Flight Control Laboratory
Extent
113
Identifier
AD0283978
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(616)-7657
DoD Project
8219
DoD Task
821901
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
Elastic-airframe dynamics, important from the standpoint of flight control system design were studied. Approximate transfer functions are given in literal terms for three classes of vehicles. These are of such a form that th important poles and zeros are related directly to simple functions of aerodynamic, elastic, and inertial properties. The aeroelastic corrections required to account for the flexibility influences of all modes not included in the equations of motions are discussed, and a rigorous method for applying these corrections is presented.
Report Availability
Full text available
Date Issued
1962-06
Provenance
Lockheed Martin Missiles & Fire Control
AFRL/VACA
Type
report
Format
1 online resource