Helicopter
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United States of America Patent
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-
Sep 27, 2016
Grant Date -
Dec 8, 2011
app pub date -
Aug 26, 2010
filing date -
Aug 26, 2009
priority date (Note) -
In Force
status (Latency Note)
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Abstract
The present invention relates to a reduced scale industrial helicopter, with an integrated automatic flight control system, that includes core autopilot functions, GPS management, and full-function navigation systems. The autopilot technology includes rapid launch capability, real-time in-flight switching between one or more of a) remote control, b) autopilot-directed, c) ground station controlled, and d) home modes, and is upgradeable. The helicopter is used for high or low altitude surveillance, and can handle various payloads, including photographic missions. The helicopter may include onboard batteries and/or a unique battery unit disposed beneath the helicopter, and includes autonomous features such as automatic takeoff, automatic landing, safety return to home base, and predetermined mission plans.
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