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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(15)

时间:2011-10-27 00:46来源:蓝天飞行翻译 作者:公务机
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NOTE
The autopilot will disengage whenever a TOGA button is pressed on the ground or in-flight. The autopilot visual and aural disengage warnings may be canceled by pushing either TOGA button again, or by pushing any AP/SP DISC switch.
With takeoff mode selected, the heading reference is continuously set to the current aircraft heading while maneuvering on the ground. After lift-off (weight off wheels), the takeoff mode generates a heading hold command, with a five-degree bank limit, using the heading which existed at the moment of lift-off. These heading references are independent of the HDG bug.
Takeoff lateral mode is cleared by selecting another lateral mode.

Lateral Takeoff Mode
Figure 04.10.26

 

 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.32 
Oct 05/06 

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


NOTE
The autopilot will disengage whenever a TOGA button is pressed on the ground or in-flight. The autopilot visual and aural disengage warnings may be canceled by pushing either TOGA button again, or by pushing any AP/SP DISC switch.
The lateral component of go-around mode (GA) generates commands to maintain the heading that existed at the moment of GA mode activation. Go-around mode generates a heading hold command with a five-degree bank limit. This heading reference is independent of the HDG bug.
Go-around mode is cleared by selecting another lateral mode.

Lateral Go-Around Mode
Figure 04.10.27

Flight Director Vertical Modes
There are nine vertical flight director modes (bold letters refer to the flight control panel button selections):
.
Pitch

.
Altitude preselect

.
Altitude hold (ALT)

.
Vertical speed (VS)

.
Flight level change (FLC)

.
Takeoff

.
Go-around

.
Glideslope

.
FMS vertical navigation (VNAV)

 


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.33 
Oct 05/06 

Vertical modes are armed or activated by the FCP push-buttons, a pitch wheel on the flight control panel, or by TOGA switches on the thrust levers. In general, disabling the active vertical mode is accomplished by reselecting the active FCP push-button, or by selecting another vertical mode.

Pitch Mode
Pitch mode (PTCH) is the basic vertical operating mode, and is automatically selected when no other vertical mode is active and the flight director is on. A green PTCH annunciation appears in the vertical active field of the FMA when pitch mode is active.
 
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