Honeywell G.m.b.h.

Honeywell International Inc.

Mark E Wright

Brian A Blow

Mark T Manfred

Stephen Matthew Baker

Randall Lynn Dodson

Tom Ryno

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.

Inertial signals for flight control backup mode

The invention is an apparatus which utilizes relatively few conductors to provide fail-safe communication between multiple electrical subsystems and a redundant pair of data processors. This is accomplished by including two first-in, first-out memory units within each electrical subsystem, and utilizing these memory units to send the output data from the electrical subsystems on a pair of parallel data buses to a redundant pair of data processors, which then perform error tests on the data to ensure its integrity.

FIFO fail-safe bus

A system for operating a pair of microprocessors with independent system clocks while at the same time providing synchronization by a common interrupt signal, and in which the system clocks are cross-monitored to thereby provide Fail-Safe operation.

Growing community of inventors

Minneapolis, MN, United States of America

Mark E Wright