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

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

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.