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Test Techniques for Flight Control Systems of Large Transport Aircraft offers theory and practice of flight control system tests. It is a systematic and practical guide, provid… Read more
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Chapter 1: IntroductionGeneralsThe current status and evolution direction for flight control system's testThe character and evaluation management for flight control system testThe requirement definition for flight control system testThe engineering practice for flight control system testThe flight control system test and validation of large transport aircraft
Chapter 2: Equipment test and validation for flight control systemGeneralsThe performance and function testIntension and rigidity testThe Power character testInsulated electricity character testMechanism condition character testEnvironment testElectromagnetism protection testReliability testDurability testTestability validationTest articles selection and sequence for airborne equipment validationOrganizing and implementation for airborne equipment validation
Chapter 3: Software test and validation for flight control systemGeneralsSoftware testingModel-based design and testFull life sustain environment for softwareTesting method for software's security and reliability
Chapter 4: Flight control law and flying qualities evaluating GeneralsPhase division and test objectiveDesign requirement of engineering simulatorThe test content and methodThe test data collection, processing and evaluating methodThe management for flight control law and flight quality evaluating test
Chapter 5: Tests of flight control subsystemGeneralsThe cockpit control subsystem integration testThe flight by wire subsystem integration testThe high lift control subsystem integration testThe automatic flight control subsystem integration testThe mechanic backup control subsystem integration test
Chapter 6: Integration and validation based on the ‘iron bird’GeneralsThe testing environment and sustain facilitiesDebugging and preparing for flight control system's integration test based on the ‘iron bird’Cockpit control device integration test based on the ‘iron bird’Mechanic backup control subsystem integration test based on the ‘iron bird’Flight by wire subsystem integration test based on the ‘iron bird’High lift control subsystem integration test based on the ‘iron bird’Automatic flight control subsystem integration test based on the ‘iron bird’Flight control system integration test and validation based on the ‘iron bird’Pilot-in-loop test based on the ‘iron bird’Evaluating method for flight control system integration test based on the ‘iron bird’The management for flight control system integration test based on the ‘iron bird’
Chapter 7: Onboard-ground aircraft test of flight control systemGeneralsThe flight control system integration test on airplaneThe structure model interaction testThe electromagnetism compatibility test on airplane
Chapter 8: Flight-test of flight control systemGeneralsThe requirement of flight control system flight-testsA general outline for flight control system flight-testThe test system for flight control system flight-testThe test data collection、processing and evaluating method for flight control system flight-testThe management for flight control system flight-test
Chapter 9: Airworthiness test and validation for flight control systemGeneralsThe certification requirement for airworthiness validationThe technology requirement for airworthing validation
Chapter 10: Current status and prospects for flight control system test and validationThe flight control system of active control aircraft and control configure vehicleThe flight control system of the aircraft with generalized control surfaceThe application of modern control theory and non-linearity control theoryThe framework of aircraft integration control systemThe framework of the flight control system based on distributed networkFlight by light control system and Flight by Wi-Fi control systemThe flight control system of more electric/all-electric aircraftThe application of the simulation equipmentFrom single system to fusion systemInformation fusion and rapid process has been essential test conditions of modern flight control systemSynchronizing the design process and test process
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