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

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Report Number: AFFDL TR 75-63
Author(s): Porter, Milton B.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1975-06
Pages: 228
Contract: Laboratory Research - No Contract
DoD Project: 8219
Identifier: ADA014301

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Provenance: AFRL/VACA

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