2
To rn ado Fli ght Control System GEC Avionics, Combat Aircraft Controls Division is responsible for the Flight Controls System for the Tornado front line combat aircraft. The system comprises: Autopilot and Flight Director System (AFDS) Command Stability Augmentation System (CSAS) Spin Prevention and Incidence Limiting System (SPILS) These high integrity equipments and th eir relationship are shown in Figure 1. The centre fold provides a summary of the equipment performance, together with a picture showing th e equipment which makes up the Flight Control System (FCS) The Tornado FCS is specifically designed to meet the rugged all-weather, day/night, low level opera- tional requirements of the aircraft. The aircraft is able to survive a single failure without operational limitation; while a second failure results in fail-safe operation. The FCS controls the rudder, tailerons and spoilers. In addition the two tailerons have mechanical reversion. ] STICK ." (Pl l CH) RATE "". G "''' Will I 1I rl I PORT ACTUAT OR ,M "'FOS "" COMPUTER' PITCH nu IAILERON I COMPl HER ST ARBOARD - ACTUATOR I "'" I AIRS TREAJoI I _I COMPUT ER OIRECTION AVIONICS AFOS C"" I DETECTOR SEN!l)RS P IlOTS PILDTS I CONT AOl CON''''' c.cM'UTEAS PANEL PANEl SPILS r--1 I PILotS INBOARD CCMROl ACTUA TORS PANEL """" I OUTBOASIO AClUAIORS AFOS CSAS COMPUTEJl2 LATERAL COMPUTER RUDDER I AC T UATOR '" 'rR-" ", J J J AUIO- I STICK THROTTLE ROLL ACtUATOO ( ROll) "''' G "" G "" PEDALS HEAD-UP I DISPLAY . Figure 1 The AFDS comprises two 3/. ATR short LRU which provide duplex digital autopilot and flight director functions. In addition to usual autopilot modes the Tornado GRl terrain following signals are pro- cessed within the AFDS to provide both automatic and manual output to the CSAS and Head Up dis- play respectivel y. The CSAS receives demand inputs either from the pilot via the stick or from At'DS . CSAS is a triplex axis-orientated system with fourth lane consolidation to meet the high safety of flight requirements of the Tornado. The CSAS is housed in two 1 ATR LRU. SPILS is housed in a \12 ATR short LRU and provides the capability for carefree aircraft handling throughout the Tornado perform- ance envelope. Over 1000 flight control systems have already been delivered. The system has been in service for ov er 10 years and has surpassed all operational performance and availability goals In the most rigor- ous environments in cluding the recent Gulf conflict. www.rochesteravionicarchives.co.uk

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Page 1: Tornado Flight Control System - rochesteravionicarchivescdn.rochesteravionicarchives.co.uk/img/catalog/ZZ_1354029405... · Tornado Flight Control System ... Combat Aircraft Controls

Tornado Flight Control System

GEC Avionics, Combat Aircraft Controls Division is responsible for the Flight Controls System for the Tornado front line combat aircraft.

The system comprises:

• Autopilot and Flight Director System (AFDS) • Command Stability Augmentation System (CSAS) • Spin Prevention and Incidence Limiting System (SPILS)

These high integrity equipments and their relationship are shown in Figure 1. The centre fold provides a summary of the equipment performance, together with a picture showing the equipment which makes up the Flight Control System (FCS)

The Tornado FCS is specifically designed to meet the rugged all-weather, day/night, low level opera­tional requirements of the aircraft. The aircraft is able to survive a single failure without operational limitation; while a second failure results in fail-safe operation. The FCS controls the rudder, tailerons and spoi lers. In addition the two tailerons have mechanical reversion.

] ~ STICK ~ ." (Pl l CH) RATE "". G"''' Will

I 1I ~ rl TAILEAO~

I PORT ACTUATOR

,M "'FOS "" COMPUTER' PITCH nu

IAILERON I COMPlHER STARBOARD - ACT UATOR

I "'" ~ I AIRS TREAJoI I _I COMPUTER OIRECTION

AVIONICS AFOS C"" I DETECTOR SEN!l)RS P IlOTS PILDTS

I • CONTAOl CON''''' c.cM'UTEAS PANEL PANEl

SPILS r--1 ,~'" I ~

PILotS INBOARD CCMROl ACTUATORS PANEL

"""" I OU TBOASIO AClUAIORS

AFOS CSAS COMPUTEJl2 LATERAL COMPUTER RUDDER I AC TUATOR

'" 'rR-" ",

J J J AUIO-

I STICK THRO TTLE

ROLL ~:lt ACtUATOO

( ROll) "''' • G"" G"" PEDALS

HEAD-UP I DISPLAY . Figure 1

The AFDS comprises two 3/. ATR short LRU which provide duplex digital autopilot and flight director functions. In addition to usual autopilot modes the Tornado GRl terrain following signals are pro­cessed within the AFDS to provide both automatic and manual output to the CSAS and Head Up dis­play respectively. The CSAS receives demand inputs either from the pilot via the stick or from At'DS. CSAS is a triplex axis-orientated system with fourth lane consolidation to meet the high safety of flight requirements of the Tornado. The CSAS is housed in two 1 ATR LRU. SPILS is housed in a \12 ATR short LRU and provides the capability for carefree aircraft handling throughout the Tornado perform­ance envelope.

Over 1000 flight control systems have already been delivered. The system has been in service for over 10 years and has surpassed all operational performance and availability goals In the most rigor­ous environments including the recent Gulf conflict.

www.rochesteravionicarchives.co.uk

Page 2: Tornado Flight Control System - rochesteravionicarchivescdn.rochesteravionicarchives.co.uk/img/catalog/ZZ_1354029405... · Tornado Flight Control System ... Combat Aircraft Controls

GEe Avionics Limited Combat Aircraft Controls Division Airport Works. Aochester, Kent ME1 2XX. England

Telephone: Medway 10634) 844400 Telex : 94017803-CACD G Faesmile: 10634) 816525

Associate Company: GEe Avlonics Inc. 2975 Northwoods Parkway /Norcross P,Q. Box 81999. Atlanta . Georgia 30366. USA

Telephone: 1404) 448 1947 Telex: 708447 Faesmlle : 1404) 246 0378

GEe Avionics Limited is a subsidiary of the General Electric Cornpan ~' of England CopyriGht © GEe Avionics Limited 1984

This bl'ochure Is Intended only to give a gene.·BI imllr6!is\on of the products and services which Brc avallahle and none of the descrlvllons contll.lntlt.l her~ln shall form IJart of any contract