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canadair chauenQer OPERATING MANUAL SECTION 4 AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS S u b j e c t ZiSi GENERAL 1 FLIGHT DIRECTOR SYSTEM 1 AIR DATA SYSTEM 2 AUTOPILOT SYSTEM '- STABILITY AUGMENTATION SYSTEM ? Yaw Damping Mach Trim FLIGHT DIRECTOR COMPONENTS 7 Attitude Director Indicator Horizontal Situation Indicator Remote Heading and Course Select Controller Flight Director Mode Selector Flight Director Computer $ Rate Gyro Vertical Gyro Directional Gyro Instrument Comparator Touch Control Steering AIR DATA COMPONENTS 3 Air Data Computer P i l o t ' s Altimeter 9 P i l o t f s Vertical Speed Indicator P i l o t ' s Mach/Airspeed Indicator TAS/SAT/TAT Indicator VNAV Computer/Controller RIGHT COMPARTMENT DISPLAYS 9 Attitude Director Indicator Attitude Sphere Aircraft Symbol 12 Roll Attitude Pointer Eyelid Display Pitch and Roll Command Bar Flight Director Warning Flag Glideslope Pointer Glideslope Warning Flag 4 - CONTENTS Page 1 Oct 03/83 cacnhaatiiiaeinr Qer OPERATING MANUAL Subject Page FLIGHT COMPARTMENT DISPLAYS Radio Altitude Bar 12 Expanded Localizer Pointer 13 Inclinometer Attitude Test Switch Speed Command Display Rate-of-Turn Rate-of-Turn Warning Flag Attitude Warning Flag Localizer Warning Flag 14 Speed Command Warning Flag Mode Annunciators Radio Altitude Display Decision Height Set Knob and Dim Control Radio Altitude Test Switch Decision Height Display 15 Horizontal Situation Indicator Aircraft Symbol Heading Dial Heading Bug Heading Flag Course Select Pointer 18 Course Display Course Deviation Bar Course Deviation Dots Vertical Deviation Pointer Vertical Warning Flag Distance Display NAV Mode Annunciator 19 RNAV Mode Annunciator Alert Annunciator Vertical Mode Annunciator Bearing Pointer Bearing Select Pushbuttons and Annunciators True Heading Annunciator Navigation Warning Flag 20 Compass Sync Annunciator Navigation Source Annunciators To-From Annunciator Instrument Remote Controller Pilot's Altimeter Altitude Alert 23 Failure Warning Flag Pilot's Vertical Speed Indicator Pilot's Mach/Airspeed Indicator TAS/SAT/TAT Indicator VNAV Computer/Controller Altitude Preselect Altitude Alert 24 4 - Page Oct canadair chauenQer OPERATING MANUAL Subject fii? FLIGHT COMPARTMENT DISPLAYS Vertical Navigation Computation 24 Vertical Path Flying 29 Vertical Input Cancelling Instrument Comparator SYSTEM CONTROLS 29 Flight Director Mode Selector Heading Select Mode 30 Navigation Mode VOR Mode VOR Approach Mode 33 RNAV Mode Localizer Mode Back Course Mode Localizer Approach Mode 34 Pitch Hold Mode Altitude Hold Mode Indicated Airspeed Hold Mode 36 Vertical Speed Hold Mode Mach Hold Mode Standby Mode Altitude Preselect Mode 37 VNAV Mode Go-Around Mode Touch Control Steering Autopilot Controller 33 Yaw Damper Engage Autopilot Engage Turn Knob Pitch Hold Couple 41 Soft Ride FAILURE MONITORING AND STATUS ANNUNCIATION 41 Failure Warnings Autopilot Self-Test 43 4 - Page Oct canadsir chanentjer OPERATING MANUAL LIST OF ILLUSTRATIONS Figure Number Title Page 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 AFCS Flight Compartment Contro" Stability Augmentation Control Attitude Director Indicator (2 Horizontal Situation Indicator Instrument Remote Controller Altimeter Vertical Speed Indicator Mach/Airspeed Indicator TAS/SAT/TAT Indicator VNAV Computer/Controller Instrument Comparator Flight Director Mode Selector Control Wheel Throttle Actuating Lever Autopilot Controller Warning and Disengage Lights Autopilot Status Panel Is and Indicators Panel Sheets) (2 Sheets) 3/4 6 10 16 21 22 25 25 27 28 31 32 35 39 40 42 44 canaaair chauencier OPERATING MANUAL SECTION 4 AUTOMATIC FLIGHT CONTROL SYSTEM GENERAL (Figure 1) www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier-Challenger_00-Automatic_Flight_Control_System
