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庞巴迪挑战者605公务机机组操作手册 CL605-AUTOMATIC_FLIGHT_CONTROL_SYSTEM(14)

时间:2011-10-27 00:46来源:蓝天飞行翻译 作者:公务机
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With approach mode armed (APPR button selected on FCP) during localizer intercept, the active navigation source will automatically change from FMS to LOC (automatic NAV to NAV transfer) at localizer capture. If required, approach mode can then be canceled and navigation mode selected by pressing the NAV button on the FCP.


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.26 
Oct 05/06 


ILS Approach Mode
Figure 04.10.23

 


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.27 
Oct 05/06 

FMS-Based Approach
Pushing the APPR button alternately selects and clears approach mode. The FMS-based approach mode functions the same as FMS navigation (LNV) mode. Additionally, glide path (GP) mode is armed for capture, to track the desired glide path from the FMS if VNAV is selected.
Refer to the Collins FMS–6000 Flight Management System Pilot’s Guide for additional information on FMS-based approaches.


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.28 
Oct 05/06 


FMS Approach Mode
Figure 04.10.24

 


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.29 
Oct 05/06 


Localizer Back Course Mode
Back course mode (B/C) generates commands to track a localizer signal using reverse-sensing.
Back course mode is armed by pressing the B/C button on the FCP. Back course mode localizer capture is the same as NAV mode; B/C1 (or B/C2) shows in white in the armed lateral mode field on both PFDs. When armed, the FCC operates in a heading select submode until capture of the localizer occurs.
If the back course approach is selected from the FMS, the localizer frequency is tuned automatically and the course display is set to the appropriate inbound course. With back course mode armed, the active navigation source will automatically change from FMS to LOC (automatic NAV to NAV transfer) at localizer capture.
After capture, the FCC generates commands to track the reciprocal of the selected course. The front course track must be set in order to have valid B/C guidance. Capture of the back course is indicated by a green B/C1 or B/C2 in the active field of the FMA. Glideslope is inhibited when B/C mode is active.
Back course mode is cleared by selecting another lateral mode, or by changing the active side navigation source or frequency.


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.30 
Oct 05/06 


Back Course Mode
Figure 04.10.25

 


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.31 
Oct 05/06 


Lateral Takeoff
On the ground, pushing either TOGA (takeoff/go-around) button, mounted on the thrust levers, selects takeoff mode and clears all other lateral modes. Lateral and vertical takeoff mode selections are coincident. When takeoff mode is active, a green TO appears in the active lateral field of the FMA. During takeoff mode, the flight directors operate in dual independent mode.
 
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