Results of study of propulsion system/control system interface for several V/STOL hover control concepts in aircraft using lift plus lift-cruise propulsion concept; control concepts included are proportional reaction controls using lift engine compressor bleed air, engine thrust modulation, and engine thrust vectoring; effects on control system performance of reaction control thrust augmentation by duct burning are shown; concepts are applied to three subsonic V/STOL strike-reconnaissance fighter aircraft of different gross weights, and comparison of concepts on basis of bleed air requirements, thrust-to-weight ratio penalties, and lift engine operating limitations is made.
V/STOL hover control system analysis
J Aircraft
Journal of Aircraft ; 3 , n 5
1966
9 pages
Article (Journal)
English
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V/STOL hover control system analysis
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