Rockwell Collins, Inc.

Douglas L Bader

Mark Clifford Singer

Mark A Kovalan

Douglas Robert Johnson

John W Roltgen

Zafar S Ahmad

John William Roltgen, Iii

A system includes a first plurality of processors, a second plurality of processors dissimilar from the first plurality of processors, a first arbitration device coupled to the first plurality of processors, and a second arbitration device coupled to the second plurality of processors. The first arbitration device and the second arbitration device is configured to receive event data, store the received event data, and to output the received event data at substantially a same time. At least one processor of the first plurality of processors and at least one processor of the second plurality of processors are configured to access the event data.

Synchronization mechanisms for high-integrity computing

A system and method are provided for controlling aircraft flight control surfaces. The system may include at least three pilot sensor channels, each pilot sensor channel including a set of pilot sensor data. The system may also include at least three aircraft sensor channels, each aircraft sensor channel including a set of aircraft sensor data. The system may further include an actuator control component configured to synchronously receive and vote on the pilot sensor data and the aircraft sensor data, such that a voted output of the at least three pilot sensor channels is transmitted to a flight control computer and augmented before being transmitted to remote electronics units. The voted output of the at least three pilot sensor channels providing for the control of the aircraft surfaces coupled to the remote electronics units.

Triplex cockpit control data acquisition electronics

Growing community of inventors

Cedar Rapids, IA, United States of America

Douglas L Bader