Dynon Avionics SkyView Скачать руководство пользователя страница 8 | Manualshive

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Dynon Avionics SkyView Скачать руководство пользователя страница 8

Autopilot

In

‐

Flight

Tuning

Procedures

1

‐

8

SkyView

Autopilot

In

‐

Flight

Tuning

Guide

‐

Revision

A

Detailed

Explanation

1.

Establish

trimmed

level

flight

on

a

fixed

heading

You

should

start

the

procedure

by

placing

the

aircraft

in

level

flight,

in

neutral

trim,

on

a

fixed

heading.

Try

to

maintain

a

constant

heading

during

the

procedure.

2.

Engage

the

Flight

Director

(FD)

in

TRK

and

IAS

mode

To

engage

the

flight

director

in

TRK

and

IAS

mode:

1.

Enter

the

AP

Menu

(MAIN

MENU

>

AP)

2.

Press

the

FD

button

3.

Press

button

4,

ROLL,

then

button

3,

TRK

a.

It

should

be

highlighted

and

look

like

4.

Press

the

BACK

button

5.

Press

button

5,

PITCH,

then

button

3,

IAS

a.

It

should

be

highlighted

and

look

like

6.

Example:

if

the

Flight

Director

were

engaged

in

TRK

mode

on

a

TRK

of

360

degrees

and

an

IAS

of

100,

the

top

bar

would

look

like

this:

a.

3.

Engage

the

Autopilot

(AP)

To

engage

the

autopilot:

1.

Enter

the

AP

Menu

(MAIN

MENU

>

AP)

2.

Press

AP

3.

The

AP

and

FD

buttons

should

look

like

4.

Allow

a

few

minutes

of

stable

flight

under

AP

control

Ensure

that

you

are

not

affecting

the

autopilot’s

control

of

the

pitch

axis,

so

you

can

determine

the

autopilot’s

IAS

hold

performance.

5.

Increase

IAS

target

by

10

knots

Change

the

IAS

bug

to

10

knots

above

the

current

IAS

target.

1.

Configure

a

joystick

to

control

the

IAS

bug.

The

label

above

the

joystick

should

read

(IAS).

2.

Turn

the

joystick

clockwise

until

the

IAS

bug

reads

10

knots

higher

than

it

did

when

the

Flight

Director

was

engaged.

3.

The

aircraft

should

immediately

begin

descending

toward

the

new

IAS

target.

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Содержание SkyView

Страница 1: ... great visibility no airspace conflicts etc If possible bring someone along on the first autopilot test flight If autopilot behavior performance or interference with the controls is cause for concern while flying remember that the autopilot can be disconnected in any of the following ways Press the Disconnect CWS button If using the SIMPLIFIED controls o Enter the AP Menu MAIN MENU AP MENU and pre...

Страница 2: ...K target 90 degrees from the current target 5 Check for ROLL SLIP indications a If observed disconnect AP increase ROLL TORQUE by 10 and start over b If ROLL TORQUE is already set to 100 contact Dynon 6 Check if aircraft is slow to respond a If observed disconnect AP increase ROLL SENSITIVITY by 2 and start over b If ROLL SENSITIVITY is already maxed out contact Dynon 7 Check if aircraft is twitch...

Страница 3: ...Autopilot In Flight Tuning Procedures SkyView Autopilot In Flight Tuning Guide Revision A 1 3 Detailed Flowchart Figure 1 Roll Axis Flight Test Procedure ...

Страница 4: ...e heading bug The label above the joystick should read TRK 2 Turn the joystick either way until the track bug reads 90 degrees to the left or right of current TRK target 3 The aircraft should immediately begin turning toward the new TRK target 5 Check for ROLL SLIP indications Observe the autopilot status indicator on the Top Bar while the autopilot flies If the banner is shown frequently it is an...

Страница 5: ...Check if aircraft overshoots TRK target Observe if the autopilot is overshooting or wandering around the track target The autopilot should keep the open triangle of the track bug closely aligned with the small magenta ground track triangle If an overshoot is observed and you made a recent ROLL GAIN adjustment disconnect the autopilot increase ROLL GAIN by 0 2 SETUP MENU AUTOPILOT SETUP ROLL AXIS G...

Страница 6: ...served disconnect AP increase PITCH TORQUE by 10 and start over b If PITCH TORQUE is already set to 100 contact Dynon 7 Check if aircraft lags FD command bars a If observed disconnect AP increase PITCH SENSITIVITY by 2 and start over b If ROLL SENSITIVITY is already maxed out contact Dynon 8 Check if aircraft is twitchy in PITCH axis a If observed decrease PITCH SENSITIVITY by 1 b Increase IAS tar...

Страница 7: ...Autopilot In Flight Tuning Procedures SkyView Autopilot In Flight Tuning Guide Revision A 1 7 Detailed Flowchart Figure 2 Pitch Axis IAS Hold Flight Test Procedure ...

Страница 8: ...ed and look like 6 Example if the Flight Director were engaged in TRK mode on a TRK of 360 degrees and an IAS of 100 the top bar would look like this a 3 Engage the Autopilot AP To engage the autopilot 1 Enter the AP Menu MAIN MENU AP 2 Press AP 3 The AP and FD buttons should look like 4 Allow a few minutes of stable flight under AP control Ensure that you are not affecting the autopilot s control...

Страница 9: ...ng and are still observing unacceptably slow behavior contact Dynon for assistance 8 Check if aircraft is twitchy in PITCH axis Observe if the flight controls twitch excessively or seem overly aggressive If it does this is an indication that the PITCH SENSITIVITY needs to be decreased Decrease PTICH SENSITIVITY by 1 SETUP MENU AUTOPILOT SETUP PITCH AXIS SENSITIVITY There is no need to disconnect t...

Страница 10: ...g to 10 knots below the current IAS target 1 Configure a joystick to control the IAS bug The label above the joystick should read IAS 2 Turn the joystick counter clockwise until the IAS bug reads 10 knots lower than it did when the Flight Director was engaged 3 The aircraft should immediately begin climbing toward the new IAS target At this point return to step 6 to re verify the settings above 12...

Страница 11: ... 100 100 PITCH SENSITIVITY 1 24 10 PITCH DEFAULT CLIMB VERT SPD 100 ft min 3000 ft min 500 ft min PITCH DEFAULT DESCENT VERT SPD 100 ft min 3000 ft min 500 ft min PITCH MAXIMUM AIRSPEED 1 30 Vs1 0 95 Vn0 0 90 Vn0 PITCH MINIMUM AIRSPEED 1 30 Vs1 0 95 Vn0 1 35 Vs1 PITCH PITCH GAIN 0 1 3 0 2 0 PITCH ALTITUDE GAIN 0 1 2 5 0 6 PITCH VSI GAIN 0 10 2 50 0 6 PITCH PULL RATE 1 0 2 0 1 0 PITCH G ERROR LIMIT...

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