The patent relates to an apparatus that improves external load modal damping, provides the pilot command control augmentation of the load, and minimizes pilot induced oscillation, and is universally adaptable to a wide variety of helicopters. The apparatus contemplates rigid pendants which damp load motion in response to a sensor.
External Load Stabilization Apparatus
1974
9 pages
Report
No indication
English
External Load Stabilization Control Laws For An H-6 Helicopter Testbed
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