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DESCRIPTION General 04−10−1 Guidance Panel 04−10−2 Autopilot System 04−10−4 Autopilot 04−10−5 Yaw Damper 04−10−6 Autopilot Engage 04−10−7 Autopilot Disengage 04−10−8 PFD Annunciation 04−10−9 Flight Director (FD) 04−10−11 Flight Director Modes 04−10−12 Modes of Operation: (Lateral) 04−10−13 Roll (ROL) Mode 04−10−13 Heading Select (HDG) Mode 04−10−13 Lateral Navigation Modes 04−10−14 Very High Frequency OmniDirectional Range (VOR) Mode 04−10−15 Localizer (LOC) Mode 04−10−17 FMS Lateral Navigation (LNAV) Mode 04−10−19 Back Course (BC) Mode 04−10−21 Modes of Operation: (Vertical) 04−10−23 Pitch Hold (PIT) 04−10−23 Vertical Speed (VS) Select 04−10−23 Altitude Select (ASEL) Mode 04−10−24 Altitude Hold (ALT) Mode 04−10−24 Flight Level Change (FLC) Mode 04−10−25 Vertical Navigation (VNAV) Mode 04−10−27 MultiAxis Modes 04−10−28 Approach (LOC/GS, VAPP) Modes 04−10−28 ILS 04−10−28 VOR Approach (VAPP) Mode 04−10−28 Approach Mode 04−10−29 TakeOff (TO) Mode 04−10−30 Go Around (GA) Mode 04−10−30 Automatic Emergency Descent Mode (EDM) ( Optional) 04−10−32 Autopilot − Flight Director EICAS Messages 04−10−34 AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS CHAPTER 4 04−00−1 Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 04−00−1 Page TABLE OF CONTENTS EMS CIRCUIT PROTECTION CB − AFCS System 04−20−1 AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS Flight Crew Operating Manual Rev 2A, Apr 11, 2005 CSP 700−5000−6 Volume 2 04−00−2 Page GENERAL The Automatic Flight Control System (AFCS) provides dual channel autopilots, dual yaw dampers, dual flight directors and automatic pitch trim. The autopilot and yaw damper functions, operate in an active standby mode, with only one channel active at a time. All computations are performed by 2 Flight Guidance Computers (FGC), located in the Integrated Avionics Computer (IAC). The FGC receives inputs from the Electronic Flight Instrument System (EFIS), the Air Data Computers (ADC), from the Inertial Reference System (IRS), from the Flight Management System (FMS), from the Fault Warning Computer (FWC) and the Data Acquisition Unit (DAU). Selection for all AFCS functions are made on the guidance panel, located on the glareshield. Guidance Panel GF0410_001 SPD PUSH CHG CRS 1 FMS MAN PUSH DCT HDG PUSH SYNC DN UP ALT CRS 2 PUSH DCT The AFCS functions controlled by the FGC include: · Flight director modes. · Guidance references. · Engagement of the autopilot and yaw damper functions. · Selection of left or right Primary Flight Display (PFD) data to be used by FGC. Through the flight computer, the AFCS will provide flight guidance outputs for display on the Primary Flight Display (PFD). The flight director functions are as follows: · Mode selection. · Computation of guidance. · Data management and source selection. · Command bar output for display. If an autopilot/flight director mode is armed or engaged, the annunciator on the appropriate button is illuminated. Indicates HDG mode is armed or engaged Indicates FLC mode is armed or engaged GF0410_002 FLC HDG SPD PUSH CHG FMS MAN HDG PUSH SYNC AUTOMATIC FLIGHT CONTROL SYSTEM Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 04−10−1 GUIDANCE PANEL Speed (SPD) Button Used to set speed on PFD (manually or by use of FMS). MAN Airspeed reference set by turning inner knob. FMS Airspeed reference set by FMS. PUSH CHG When inner knob pushed, changes IAS to Mach or Mach to IAS. Flight Director (FD) Switch Used to remove flight director command bars from the PFD not selected by the flight director. Flight Level Change (FLC) Switch Used to select airspeed hold mode. Overrides all active vertical www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Automatic_Flight_Control_System
