Air data magnetometer data, Gps data magnetometer data air data, System overview – Garmin G1000 King Air C90GT User Manual

Page 32: Gps input failure

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190-00663-01 Rev. A

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT

18

SYSTEM OVERVIEW

SY

STEM

O

VER

VIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO P

ANEL

& CNS

FLIGHT

MANA

GEMENT

HAZARD

AV

OID

ANCE

AFCS

ADDITIONAL FEA

TURES

APPENDICES

INDEX

In addition to using internal sensors, the GRS 77 AHRS uses GPS information, magnetic field data and air

data to assist in attitude/heading calculations. In normal mode, the AHRS relies upon GPS and magnetic
field measurements. If either of these external measurements is unavailable or invalid, the AHRS uses air
data information for attitude determination. Four AHRS modes of operation are available (see Figure 1-13)
and depend upon the combination of available sensor inputs. Loss of air data, GPS, or magnetometer sensor
inputs is communicated to the pilot by message advisory alerts.

Attitude/Heading Invalid

AHRS

no-GPS

Mode

AHRS Normal

Operation

AHRS no-

Mag Mode

AHRS no-Mag/

no-Air Mode

Heading Invalid

av

ailab

le

av

ailab

le

una

vailab

le

una

vailab

le

av

ailab

le

una

vailab

le

una

vailab

le

av

ailab

le

Air Data

Magnetometer Data

una

vailab

le

av

ailab

le

GPS Data

Magnetometer Data

Air Data

Figure 1-13 AHRS Operation

GPS INPUT FAILURE

NOTE:

In-flight initialization of AHRS, when operating without any valid source of GPS data and at true

air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it
is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an
extended period of time where valid AHRS outputs are unavailable.

The G1000 system provides two sources of GPS information. If a single GPS receiver fails, or if the

information provided from one of the GPS receivers is unreliable, the AHRS seamlessly transitions to using the
other GPS receiver. An alert message informs the pilot of the use of the backup GPS path. If both GPS inputs
fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer
inputs are available and valid.

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