Gpss, Straight – Dynon Avionics SkyView Pilots Users Guide User Manual

Page 175

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Autopilot Operation

SkyView Pilot’s User Guide - Revision S

8-9

immediately turning the bug turned 180° from the current track. The autopilot will turn the
aircraft to the left.

To disengage the autopilot press either the OFF button or TRK+ALT button.

Messages (Text Varies)

The Message Alert Area is always present above the rightmost button and contains important
SkyView messages and alerts.

Simplified Autopilot Modes

The following table summarizes the different autopilot modes of operation for the roll axis as
annunciated in the Top Bar.

Mode

Annunciation

Description

Track Hold

(TRK)

TRK

042

Track hold mode keeps the aircraft flying in a particular

direction, as determined by the GPS’s ground track, or

direction of travel over the ground. This target is reflected by

the track (TRK) bug in the HSI. When the autopilot is initially

engaged, the TRK bug will automatically be synchronized to

the current ground track of the aircraft. Effectively, this means

that the autopilot will keep flying in the same direction that

the aircraft was flying in the moment before the autopilot was

engaged. After the autopilot is engaged, change the track you

want the autopilot to fly by adjusting the TRK bug.

HSI (GPS)

GPS

In HSI mode, the autopilot will fly the lateral course guidance

that is displayed on the HSI from the provided source. For

example, if the selected HSI source is the SkyView GPS, and

there is an active Flight Plan, the autopilot will fly that flight

plan. Or if the source is a VOR the autopilot will seek to

capture and hold the set CRS to or from the VOR. If the HSI

source provided GPS roll steering commands (GPSS) the

autopilot will follow those commands.

HSI (GPSS)

GPSS

HSI (VOR)

VOR

HSI (LOC)

LOC

Level Mode

STRAIGHT

Holds the aircraft in a wings level attitude (zero degrees roll).

Figure 180 - Simplified Autopilot Roll Modes

The following table summarizes the different autopilot modes of operation for the pitch axis.

Mode

Annunciation

Description

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