Model based sensor system for loads aware control laws

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Reexamination Certificate

active

07970498

ABSTRACT:
A flight control system includes a model-based sensor system which estimates angular accelerations to control rotor system moment such that loads on the aircraft structure are reduced to thereby allow an aircraft structural envelope to more closely follow an aircraft service flight envelope.

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International Search Report for International Appl. No. PCT/US2008/065229 dated Jun. 29, 2009.

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