Difference between revisions of "Eurofighter Typhoon: Flight Manual"
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== Introduction == | == Introduction == | ||
+ | The Eurofighter Typhoon is an agile, multirole combat aircraft designed upon relaxed stability principles. | ||
=== Acknowledgements === | === Acknowledgements === | ||
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== Flight Controls == | == Flight Controls == | ||
+ | The aircraft is controlled via stick, throttle and rudder pedals, whose motions are processed by the Flight Control System and appropriate signals are passed to the flight control surfaces, the canards, flaperons and rudder. | ||
+ | |||
+ | === Flight Control System === | ||
+ | |||
+ | The FCS can be bypassed, but this is not recommended under normal flight conditions. | ||
+ | |||
+ | == Avionics == | ||
== Navigation == | == Navigation == | ||
+ | === Nav Aids === | ||
+ | Navigational assistance is provided by the Navigation Computer, guiding the pilot along a heading, route or beam using information from the two primary navigation systems, Route Manager and TACAN. Relevant information is displayed on the Head Up Display | ||
=== Autopilot === | === Autopilot === | ||
== Avionics == | == Avionics == |
Revision as of 15:49, 28 June 2011
This document is a work in progress. We aim to produce a concise guide to flying the Eurofighter Typhoon and operating its systems. Keep checking back - as things are added to the aircraft, so they'll be documented here - we hope to make these updates in a timely manner, ideally when new versions of the aircraft are released.
Contents
Introduction
The Eurofighter Typhoon is an agile, multirole combat aircraft designed upon relaxed stability principles.
Acknowledgements
Eurofighter Typhoon for FlightGear was developed by Maverick Alex, DFaber, Almursi, Algernon and other contributors. This document initialised by --Algernon 16:28, 28 June 2011 (EDT)
Develop & Cusomise
See Eurofighter Typhoon: Development Documentation
Flight Controls
The aircraft is controlled via stick, throttle and rudder pedals, whose motions are processed by the Flight Control System and appropriate signals are passed to the flight control surfaces, the canards, flaperons and rudder.
Flight Control System
The FCS can be bypassed, but this is not recommended under normal flight conditions.
Avionics
Navigational assistance is provided by the Navigation Computer, guiding the pilot along a heading, route or beam using information from the two primary navigation systems, Route Manager and TACAN. Relevant information is displayed on the Head Up Display