Analysis and preliminary design of an advanced technology transport flight control system, Volume 2490
Ronald Frazzini, Darrel Vaughn, Honeywell Inc. Government and Aeronautical Products Division, Langley Research Center
National Aeronautics and Space Administration, 1975 - Science - 407 pages
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FCS FUNCTIONAL CAPABILITIES
13 other sections not shown
accelerometer aircraft analog analog signal application attitude autopilot basic bits candidate configurations capability command COMPARISON MONITOR component computer configuration control surface control wheel crossfeed deadband detection device Digital Computation disengaged driver actuator electrical electronics failure rates feedback flight control system flight hour flutter fly-by-wire four channels Functional Block Diagram Functional Redundancy Block GEMM program general-purpose gyros hardware hexad Honeywell hydraulic implementation in-line monitoring included input Input/output INTEGRATED ACTUATOR integrated circuit interface LARGE PROCESSOR life-cycle cost List Printout load logic machine maintenance mechanization memory midspan mode module MPLX MTBF multiplexed operational reliability output panel percent performed pickoffs Pitch Production Cost QUAD Redundancy Block Diagram repair RRIAL Section SENSOR GROUP servo servovalve shown in Figure SIGNAL SELECT stockage Success Path Diagram support costs surface actuator switching synchronization techniques test equipment TOTAL FUNCTION tradeoff transfer function TRIPLE