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 NAVIGATION SYSTEMS Table of Contents  Vol. 2  17.00.5 
Oct 05/06 

Page 
LIST OF ILLUSTRATIONS 
DESCRIPTION 
Figure 17.10.78  CDU Message Display  17.10.84 
Figure 17.10.79  PFD Message Display  17.10.85 
Figure 17.10.80  MFD Message Display  17.10.86 

 NAVIGATION SYSTEMS Table of Contents  Vol. 2  17.00.6 
Oct 05/06 

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CL.605 Flight Crew Operating Manual
PSP 605.6

 NAVIGATION SYSTEMS Description  Vol. 2  17.10.1 
Oct 05/06 

The navigation systems calculate and display the attitude, altitude and position of the aircraft, based on data from other aircraft systems, ground stations, and sensed environmental conditions around the aircraft. The displayed information includes aircraft movement, distance, speed and direction of travel about all three axes. The present position and computed future positions can also be displayed.
This chapter will cover:
.
Inertial reference system (IRS)

.
Weather radar system

.
Terrain awareness warning system (TAWS)

.
VHF navigation system

.
Distance measuring equipment (DME) system

.
Automatic direction finder (ADF) system

.
ATC transponder

.
Traffic alert and collision avoidance system (TCAS II)

.
Global positioning system (GPS)

.
Flight management system (FMS)

INERTIAL REFERENCE SYSTEM (IRS)
Description

The Honeywell Laseref V micro inertial reference system (IRS) uses digital ring laser gyros to compute attitude, heading, angular rates, linear accelerations, vertical velocity and present position information. The IRS interfaces with the following aircraft systems:
.
Electronic flight instrumentation system (EFIS);

.
Weather radar;

.
Automatic flight control system (AFCS);

.
Flight data recorder (FDR);

.
Terrain awareness warning system (TAWS);

.
Traffic alert and collision avoidance system (TCAS);

.
Stall protection system (SPS);

.
Aircraft fuel system; and

.
Flight management system (FMS).

Alignment

The IRS requires an initialization process that establishes the relationship between the aircraft body frame and the local geographic reference. Thus, a valid input of initial latitude and longitude is necessary in order to achieve this initialization process or alignment.
　
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