The Effects of Stability Augmentation on the Gust Response of a STOL Aircraft During a Curved Manual Approach

Item

Title
The Effects of Stability Augmentation on the Gust Response of a STOL Aircraft During a Curved Manual Approach
Date
1975
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
AFFDL TR 75-63
Corporate Author
Air Force Flight Dynamics Laboratory
Laboratory
Air Force Flight Dynamics Laboratory
Date Issued
1975-06
Extent
228
Identifier
ADA014301
Access Rights
Approved for public release; distribution unlimited
Distribution Classification
1
Contract
Laboratory Research - No Contract
DoD Project
8219
DoD Task
None Given
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
report
Format
1 online resource
Creator
Porter, Milton B.