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1 Ing Ivan Ramirez Centro de ensayos de Airbus en Toulouse-Francia Automatización del Airbus en el mundo de la aviación

2 Fly by wire aircraft Page 2

3 Contents Fly by wire principles Flight Handling Page 3

4 Fly by Wire principles Page 4

5 Fly by wire principles With conventional aircraft (A , A310), pilot orders are transferred along cables, until they reach the control surface to be moved. Page 5

6 Fly by wire principles With conventional aircraft (A , A310), pilot orders are transferred along cables, until they reach the control surface to be moved. A320, A330 & A380 families : the cables have been replaced by electrical wires : FLY BY WIRE. Page 6

7 The Sidestick In fly by wire aircraft, manual roll and pitch are controlled by the side-sticks. Page 7

8 Flight Handling Page 8

9 Flight handling Conventional aircraft : a control input A surface deflection The aircraft reaction depends on speed, altitude, etc Page 9

10 Flight handling Fly by wire aircraft : a stick input COMPUTERS Load Factor Optimum control of the aircraft Roll Rate A Nz load factor demand for pitch (not a pitch angle) A roll rate demand (an angle). Page 10

11 Flight handling Computers process the electrical signal created by pilot orders. COMPUTERS PRIM 1A/1B PRIM 2A/2B PRIM 3A/3B SEC 1 SEC 2 SEC 3 SLATS / FLAPS protection laws, flight controls Role : To ensure the optimum flight control surface deflection. To improve safety : overspeed, stall, windshear, manoeuvre & attitude protections Page 11

12 Agenda Autoflight System Functions Navigation, Guidance and Piloting AFS Operational use : FCU FMS operational use : MFD Autoflight HMI description Operational logic : AP engagement/disengagement Operational logic : ATHR engagement/disengagement Mode operational logic A380-A350 Longitudinal Modes / Control laws /target Cruise mode sequencing Automatic approach sequencing Operations cat 2/cat 3 Page 12

13 Autoflight System functions Page 13

14 Autoflight System functions Flight Guidance (FG) provides short-term lateral and vertical guidance, including speed or Mach control, based on defined targets. Autopilot acts controls 3 axis (pitch, roll,yaw) via control surfaces and nose wheel steering to: Page 14

15 Autoflight System functions Flight Guidance (FG) and Flight Director (FD). Hold target selected by crew (entered into FCU : heading, vertical speed, altitude, ), Page 15

16 Autoflight System functions Flight Guidance (FG). Follow a flight plan managed by FMS (Climb, Cruise, Descent, Approach), Page 16

17 Autoflight System functions Flight Guidance (FG). Perform autoland and rollout until full stop Page 17

18 Autoflight System functions Flight Guidance (FG). Perform auto Go-around. Page 18

19 Autoflight System functions Flight Guidance (FG). Perform automatic Traffic Collision Avoidance System (TCAS) Page 19

20 Autoflight System functions Flight Guidance (FG). Keeps Aircraft in the flight envelope (speed protection) Page 20

21 Autoflight System functions Flight Director (FD) Flight Director provides guidance cues displayed on PFD, to enable in manual piloting to : Page 21

22 Autoflight System functions Flight Director (FD) Perform auto Go-around. Page 22

23 Autoflight System functions Flight envelope provides flight data and warning Page 23

24 Navigation, guidance and piloting Page 24

25 Navigation, guidance and piloting FLIGHT MANAGEMENT SYSTEM Navigation, Performance, Flight Planification, Guidance FLIGHT GUIDANCE & AUTO-THRUST SYSTEM Control of trajectory and speed Guidance Objectifs Sensors Rudder Elevator Spoilers Piloting Orders FLIGHT CONTROL SYSTEM Attitude, Acceleration control, Servo loops surfaces Surfaces orders Aileron Slats and Flaps Page 25

26 Navigation, guidance and piloting Page 26

27 AFS Operational use : FCU Page 27

28 AFS Operational Use : FCU To engage the Systems : Auto-pilot, Flight directors, Auto Thrust To perform the targets selections (including baro setting) To engage the modes Page 28

29 AFS Operational Use : FCU A380 Page 29

30 Flight Management System (FMS) Operational use : Multi Fonction Display (MFD) Page 30

31 FMS operational use :Multi Fonction Display (MFD) MFD on A380 & A350. Page 31

32 FMS operational use :Multi Fonction Display (MFD) KEYBOARD and CURSOR CONTROL UNIT (KCCU) Page 32

33 Autoflight HMI description Page 33

34 Autoflight HMI description HMI functions: crew situation awareness Engaged systems / Mode of operation

35 Autoflight HMI description Achievable performance

36 Autoflight HMI description Flight director : displayed on PFD

37 Autoflight HMI description Aircraft attitudes, flight parameters Lateral & vertical deviations (ILS approaches)

38 Autoflight HMI description Flight Plan and Navigation Data: displayed on Navigation Display (ND)

39 Autoflight HMI description Warnings and different alerts: visual display and aural warnings Loss of systems

40 Autoflight HMI description Warnings and different alerts: visual display and aural warnings Downgradation of capability

41 Autoflight HMI description Warnings and different alerts: visual display and aural warnings Excessive deviation

42 Operational logic : AP engagement / disengagement Page 42

43 Operational logic : AP engagement/disengagement AP engagement is performed through a dedicated FCU push button

44 Operational logic : AP engagement/disengagement AP disengagement is obtained by : With second action on FCU pushbutton

45 Operational logic : AP engagement/disengagement Action on one instinctive disconnect switch located on the side stick

46 Operational logic : AP engagement/disengagement AP disengagement is obtained by : When excessive pitch attitude (-13/25) or bank angle (+/-45) are reached

47 Operational logic : AP engagement/disengagement Flight control computers when flight envelope is exceeded

48 Operational logic : ATHR engagement / disengagement Page 48

49 Operational logic : ATHR engagement/disengagement ATHR can be engaged by Flight Control Unit (FCU) ATHR P/B or automatically engaged at Take off, Go around or Alpha floor. Page 49

50 Operational logic : ATHR engagement/disengagement ATHR is disengaged by Action on FCU P/B Page 50

51 Operational logic : ATHR engagement/disengagement ATHR is disengaged by Setting all throttle to idle (normal operation after landing) TAKE OFF and GO AROUND MCT REVERSER CLIMB IDLE Page 51

52 Operational logic : ATHR engagement/disengagement ATHR is disengaged by Action on instinctive disconnect INSTINCTIVE DISCONNECT PBs INSTINCTIVE DISCONNECT PBs Page 52

53 Mode Operational logic : A350-A380 Page 53

54 Mode operational logic A380-A350 AP/FD Lateral modes Mode NAV LOC HDG/TRACK Page 54

55 Mode operational logic A380-A350 AP/FD Vertical modes Level changes Altitude hold Mode Climb/Descent Open Climb/ Open Descent ALT ALT CRZ TCAS V/S - FPA G/S SRS Page 55

56 Cruise phase mode sequencing Page 56

57 CRUISE PHASE MODE SEQUENCING Page 57

58 Automatic approach sequencing Page 58

59 Automatic approach sequencing Page 59

60 Operations cat 2/cat 3 Page 60

61 Operations cat 2/cat 3 Decision height (DH): The height at which a Go Around (GA) must be initiated unless adequate visual reference has been established Page 61

62 Operations cat 2/cat 3 Runway Visual Range The maximum distance in the direction of takeoff or landing at which the runway, or specified lights or markers delineating it, can be seen from a position above a specified point on its centerline at a height corresponding to the average eye level of pilots at touch-down Page 62

63 Airworthiness requirements Rollout If RVR< 100m Page 63

64 Airbus S.A.S. All rights reserved. Confidential and proprietary document. This document and all information contained herein is the sole property of AIRBUS. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS S.A.S. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS S.A.S. will be pleased to explain the basis thereof. AIRBUS, its logo, A300, A310, A318, A319, A320, A321, A330, A340, A350, A380, A400M are registered trademarks. Page 64

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