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Aerodynamically stabilized instrument platformA suspension apparatus for suspending instrumentation from an airborne platform may include a generally longitudinal boom having a payload end and a tail end. Yaw and pitch stabilizers may be disposed at the tail end of the boom. A mast that may be selectively translatable on the boom may connect the boom to a tether line of the airborne platform. The payload may be attached to the payload end of the boom. The mast may be positioned axially along the boom at the center of gravity of the combination of the payload, boom, pitch stabilizer, and yaw stabilizer.
Document ID
20120010545
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Bland, Geoffrey L.
Miles, Ted K.
Date Acquired
August 26, 2013
Publication Date
June 12, 2012
Subject Category
Aircraft Stability And Control
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,196,853
Patent Application
US-Patent-Appl-SN-12/779,494
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