Investigation of dynamic behavior of peripheral jet over land was conducted at Aeronautical Engineering Dept of Princeton University; ground effect machine (GEM) configurations and various means of aerodynamic stabilization; analytical approach followed in paper to determine stability derivatives in hover was that of momentum balance; it is shown that control system that employs attitude and rate feedback can improve GEM stability at altitudes otherwise dangerous, and at speeds where aerodynamic control surfaces are not effective.
Design GEM stability augmentation systems
Astronautics Aerospace Eng
Astronautics and Aerospace Engineering ; 1 , n 6
1963
8 pages
Aufsatz (Zeitschrift)
Englisch
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Mixed Linear-Quadratic-Eigenstructure Strategy for Design of Stability Augmentation Systems
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