Design of FBW Flight Control Systems for Modern Combat Aircraft Shyam Chetty Former Director, CSIR-NAL Bangalore
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1 Design of FBW Flight Control Systems for Modern Combat Aircraft Shyam Chetty Former Director, CSIR-NAL Bangalore 1 IIT Dharwad
2 ABOUT TEJAS Smallest, light-weight, supersonic aircraft Designed for multiple roles Fight other aircraft & establish control over airspace: highly agile, light weight, advanced radar, BVR missiles Spying on enemy (reconnaissance): Special Infra red sensors and cameras Bombing in enemy territory: can carry multiple combination of bombs, advanced radar, stealth, fire laser guided bombs Self-defense: Radar warning receivers, chaffs, flares to fool missiles Electronic warfare: electronic counter-measures Over 4500 flights on 27 Aircraft by 26 Pilots 2
3 TEJAS 3 View - Geometry S = 38.4 m 2 b = 8.2 m AR = t/c ~ 3-4 % 50 o 62.5 o MAC = 5.6 m s max = 17.5 o, 27.5 o, 30 o -30 o to +30 o ab max = 60 o -25 o to +25 o L = 13.2 m 3
4 Required Capabilities of Combat Aircraft in Attacking Air Targets 4
5 Required Capabilities of Combat Aircraft in Attacking Ground (Surface) Objects 5
6 Fully Loaded War Machine 6
7 With Laser Guided Bombs for Precision Ground Attack LGB LDP 7
8 CONTROL CONFIGURED VEHICLE (CCV) AERODYNAMICS CONTROL ACT * STRUCTURES PROPULSION * - ACTIVE CONTROL TECHNOLOGY 8
9 SIX Degrees of Freedom of Motion LATERAL YAW AXIAL ROLL VERTICAL PITCH 9
10 Aircraft Primary Controls Rudder ( Yaw ) Engine ( Thrust) Elevator ( Pitch ) Aileron ( Roll ) 10
11 Aircraft Control (Pitch) Elevators Video 11
12 Aircraft Control (Roll) Aileron Aileron Video 12
13 Aircraft Control (Yaw) Rudder Video 13
14 CONVENTIONAL AIRCRAFT 14
15 FLY-BY-WIRE FLIGHT CONTROL Computers + Sensors Actuators 15
16 A Tale of 4 Forces & 2 Ratios 16
17 How Drag is Reduced? 17
18 How is L/D & T/W increased 18
19 Flight Control Laws Brain 19
20 FBW Flight Control Hardware 20
21 DFCC 21
22 ACTUATORS 22
23 SENSORS 23
24 FCS Software Development 24
25 TEJAS FCS OFP SOFTWARE FUNCTIONS REAL TIME EXECUTIVE (SYNCHRONIZATION, SCHEDULING) 25
26 TEJAS IFCS Test Facilities 26
27 Control Law Schematic Glimpses into the exciting world of modern aircraft design 27
28 Human Pilot Modeling & Pilot- Aircraft Coupling Glimpses into the exciting world of modern aircraft design 28
29 Control Law Block Schematic Glimpses into the exciting world of modern aircraft design 29
30 Cockpit Controls HOTAS Hands On Throttle & Stick (30 to 40 functions being controlled) 38
31 HOTAS Stick Grip 39
32 HOTAS Throttle Grip Glimpses into the exciting world of modern aircraft design 40
33 THROTTLE Grip Controls 41
34 Tejas Cockpit aircraft Ergonomics Glass Cockpit Tejas (TD1, TD2 & PV1) Tejas (PV2) 42
35 TEJAS Cockpit Glass Displays Cockpit 43
36 HUD Head Landing Up display Configuration (HUD) 44
37 Helmet Mounted Display Helmet Mounted Display 45
38 Man-Machine Interaction 46
39 Development of Multi Function Autopilot
40 Development of Multi Function Autopilot
41 Longitudinal Autopilot Modes Altitude Hold In this mode aircraft levels out in pitch (longitudinal axis) and altitude at the time level will be remembered and held. Altitude Select Pilot selects an altitude to reach and engages the mode The aircraft climbs or descents to the pilot selected altitude 42
42 Coupled Autopilot Modes Auto Level In this mode the aircraft is leveled out from unusual attitudes or from disorientation Approach Approach mode generates commands To capture and track the Localizer (LOC) To capture and hold the Glide Slope (GS) 36
43 Flight Director 37
44 H / V NAV Mode Selection 31
45 Autopilot Mode / State Transitions
46 The CLAW Design Cycle 48
47 SIMULATION PLATFORMS Engineer In Loop Pilot In Loop Inflight Simulators 49
48 Iron Bird FCS Test Rig 50
49 Iron Bird Facility 51
50 Structural Coupling Rig 52
51 Airframe Structural Modes 53
52 Test & Integration Facilities 54
53 TEJAS Lightning Tests 55
54 Work Centers of LCA Programme 56
55 Industry Participation in LCA Programme 57
56 58
57 Cold Weather Trials at -15 deg C at Leh 59
58 Amidst Majestic Himalayas Video 60
59 Hot Weather +45 deg. C Trials at Jaisalmer 61
60 Wake Clearance 62
61 Air to Air Refueling 63
62 ??? IIT Dharwad 2018
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