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庞巴迪CRJ200公务机机组操作手册 Bombardier CRJ-自动飞行控制系统(2)

时间:2011-11-17 10:49来源:蓝天飞行翻译 作者:公务机 点击:
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The flight control computerreceives mode selections from theflight controlpaneland sensor information from theair datasystem, navigation systems, attitude andheading reference system, radio altimeterand surface position sensors.
The flight control computerreceives mode selections from theflight controlpaneland sensor information from the airdata system, navigation systems,inertial reference system, radio altimeterand surface position sensors.<0025>
The FCC’s provideflightguidance commandstotheautopilot whichprovidesthe control signals to drive theaileron andelevator servos aswell asthehorizontal stabilizer trim. The flightdirector provides computed steering commands using acommandbar ontheattitude director indicatorportion ofthePFD’s. The steering commands provide visualguidance for thepilotto manually steer theaircraft as definedbythe selected modesofoperation.
Flight Crew Operating Manual  MASTER 
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 AUTOMATIC FLIGHT CONTROL SYSTEM Introduction  Vol. 1  03-
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REV 56, Jan 31/03 


Auto Flight Systems ---General
Figure 03---10---1

Flight Crew Operating Manual  MASTER 
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Vol. 1 03-
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AUTOMATIC FLIGHT CONTROL SYSTEM Introduction REV56,Jan 31/03
CLIMBMODES ROLL PITCH HDG VS
VOR SPD FMS PITCH
TAKEOFF MODE
ROLL PITCH WINGS 15DEGREES LEVEL NOSE UP HDG HOLD
CRUISE MODES 
ROLL  PITCH 
HDG  ALT SEL 
VOR  ALT HOLD 
FMS 
DESCENT MODES 
ROLL  PITCH 
HDG  PITCH 

VOR LOC FMS  VS SPD 
GS APPROACH MODES ROLL PITCH LOC VOR FMS 

GO-
AROUNDMODES ROLL PITCH HDG 10DEGREES ROLLHOLD NOSEUP
Automatic Flight Control System Modes
Figure 03---10---2

Flight Crew Operating Manual MASTER CSP A-
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 AUTOMATIC FLIGHT CONTROL SYSTEM Introduction  Vol. 1  03-
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Flight Crew Operating Manual  MASTER 
CSP A-
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 AUTOMATIC FLIGHT CONTROL SYSTEM  Vol. 1  03-
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Flight Control and Guidance  REV 56, Jan 31/03 


1. FLIGHT CONTROL AND GUIDANCE
Integration amongthe various avionics systems is providedbythe integrated avionics processingsystem (IAPS)whichis acomputercard cage locatedin the avionics compartment. Two flight control computers (FCC’s), mountedinsidetheIAPS, are the main computers fortheautomatic flightcontrolsystem(AFCS). Controllogic for thedualflight directors, thetwo axes autopilot withautomatic pitchtrim andthedualyawdampers is contained within thetwo FCCs.
The FCC’s use altitudeandheading reference system(AHRS)andair datacomputer(ADC) system information tocalculate flightpath and controlparameters forthe AFCS. Other inputsto theflight controlcomputers include selections made ontheflight controlpanel, flight management computeroutputsand radio systemoutputs.
 
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