Inertial signals for flight control backup mode

Details Inertial signals for flight control backup mode Inertial signals for flight control backup mode

2007-07-03

2011-11-29

Keith, Jack (Department: 3663)

Data processing: vehicles, navigation, and relative location

Vehicle control, guidance, operation, or indication

Aeronautical vehicle

C701S014000, C244S075100, C244S07600R

Reexamination Certificate

active

08068943

ABSTRACT:
A flight control system is provided that includes a reference system and flight control actuators. The reference system includes one or more sets of gyroscopes and accelerometers. At least one set of the gyroscopes and accelerometers are configured to provide a first output of a first set inertial signals for normal mode flight control and second output of a second different set of inertial signals for backup mode flight control. The flight control actuators are configured to be controlled by one of the first set of inertial signals and the second set of inertial signals.

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patent: 2006/0100750 (2006-05-01), Platzer et al.
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