Design of FBW Flight Control Systems for Modern Combat Aircraft Shyam Chetty Former Director, CSIR-NAL Bangalore

Similar documents
Module 2: Lecture 4 Flight Control System

ŞahinSim: A Flight Simulator for End-Game Simulations

412 th Test Wing. War-Winning Capabilities On Time, On Cost. Lessons Learned While Giving Unaugmented Airplanes to Augmentation-Dependent Pilots

Fokker 50 - Automatic Flight Control System

Status of Handling Qualities Treatment within Industrial Development Processes and Outlook for Future Needs

Digiflight II SERIES AUTOPILOTS

FROM IN-FLIGHT SIMULATORS TO UAV SURROGATES

F-104 Electronic Systems

Flight Control Law Development for the F-35 Joint Strike Fighter

User Manual Version 1.0

Classical Control Based Autopilot Design Using PC/104

UAV: Design to Flight Report

Neural Flight Control Autopilot System. Qiuxia Liang Supervisor: dr. drs. Leon. J. M. Rothkrantz ir. Patrick. A. M. Ehlert

Dash8-200/300 - Automatic Flight AUTOMATIC FLIGHT CONTROLS AND INDICATORS. Page 1

Operating Handbook For FD PILOT SERIES AUTOPILOTS

Post-Installation Checkout All GRT EFIS Models

ARKBIRD-Tiny Product Features:

Various levels of Simulation for Slybird MAV using Model Based Design

Multi-Axis Pilot Modeling

A New Perspective to Altitude Acquire-and- Hold for Fixed Wing UAVs

Module 13 Aircraft Aerodynamics, Structures and Systems

Design of a Flight Stabilizer System and Automatic Control Using HIL Test Platform

MGL Avionics. iefis. Integrated Autopilot. User and installation manual. Manual dated 14 November Page 1

Keywords: Aircraft Systems Integration, Real-Time Simulation, Hardware-In-The-Loop Testing

Aeromechanics Safety Support Team Providing Aeromechanical Engineering Resources and Support for Aircraft Incidents and Mishap Investigations

Active Inceptor Systems

Rapid Prototyping a Two Channel Autopilot for a Generic Aircraft

FLCS V2.1. AHRS, Autopilot, Gyro Stabilized Gimbals Control, Ground Control Station

Introduction. Figure 1. HOTAS Warthog joystick with FSSB R3 mod.

Flight control system for a reusable rocket booster on the return flight through the atmosphere

Digiflight II SERIES AUTOPILOTS

CHAPTER 5 AUTOMATIC LANDING SYSTEM

Seismic Simulator (Earthquake)

EMBRAER 135/145 Autopilot

SECTION 2-19 AUTOPILOT

17 Wellington Business Park Crowthorne Berkshire RG45 6LS England. Tel: +44 (0)

Flight-dynamics Simulation Tools

GPS System Design and Control Modeling. Chua Shyan Jin, Ronald. Assoc. Prof Gerard Leng. Aeronautical Engineering Group, NUS

SmartFly Cirrus Cirrus. Flight Trainer

Human Factors in Glass Cockpit Aircraft

GUIDED WEAPONS RADAR TESTING

IL 2 STURMOVIK GREAT BATTLES VERSION 3.002c 15 May 2018 Battle of Stalingrad Battle of Moscow Battle of Kuban

Table of Contents. Introduction 3. Pictorials of the 40 and 50 Systems 4. List of Applicable Acronyms 6

Page Chg

Size. are in the same square, all ranges are treated as close range. This will be covered more carefully in the next

Flight Dynamics AE426

Google Earth Tutorials

Operating Handbook. For. Gemini Autopilot

Desktop real time flight simulator for control design

Head-Up Guidance System. HGS Pilot Guide for the Bombardier CRJ 700

Implementation of Nonlinear Reconfigurable Controllers for Autonomous Unmanned Vehicles

THE RAY ALLEN COMPANY

BLACKBOARD ARCHITECTURE FOR AN UNMANNED AERIAL VEHICLE CONTROLLER USING FUZZY INFERENCE SYSTEMS SWETHA PANDHITI

University of Minnesota. Department of Aerospace Engineering & Mechanics. UAV Research Group

Safety Enhancement SE (R&D) ASA - Research Attitude and Energy State Awareness Technologies

Flight Detector Indicator

MGL Avionics EFIS. Integrated Autopilot. User and installation manual. Manual dated 24 May 2010

Fixed Wing Models 55

Artificial Neural Networks based Attitude Controlling of Longitudinal Autopilot for General Aviation Aircraft Nagababu V *1, Imran A 2

Official Journal of the European Union L 298/75

Hardware-in-the-Loop Simulation for a Small Unmanned Aerial Vehicle A. Shawky *, A. Bayoumy Aly, A. Nashar, and M. Elsayed

LOC. prevent. Simple tools to. Display Disorientation. Practical, low-cost technologies are within reach to reduce the risk of loss of control.

CATEGORY 7 - NAVIGATION AND AVIONICS A. SYSTEMS, EQUIPMENT AND COMPONENTS

FlyRealHUDs Very Brief Helo User s Manual

Lesson 17: Science and Technology in the Acquisition Process

FUZZY CONTROL FOR THE KADET SENIOR RADIOCONTROLLED AIRPLANE

The Pennsylvania State University. The Graduate School. College of Engineering

Accurate Automation Corporation. developing emerging technologies

Controller based Electronic Speed Controller for MAV Propulsion System

Rotary Wing DVE Solution Proof Of Concept Live Demonstration

AFI Flight Operations Safety Awareness Seminar (FOSAS)

The C2/C4ISR Systems Market

CDS 101/110a: Lecture 8-1 Frequency Domain Design

Ray Aviation Article. Lockheed F-35 Simulator. Simulator built by YouFly

Acquisition of HR Textron

True F-16 SPECIFICATION. Dynamic Motion Seats SHEET

Icing Encounter Flight Simulator

Jam Lab Capabilities. Charles Dionne. Matthew Pilat. Jam Lab Manager

Heterogeneous Control of Small Size Unmanned Aerial Vehicles

AIRCRAFT AVIONIC SYSTEMS

Page Chg

Roll Control for a Micro Air Vehicle Using Active Wing Morphing

Skylark OSD V4.0 USER MANUAL

OughtToPilot. Project Report of Submission PC128 to 2008 Propeller Design Contest. Jason Edelberg

Design and Implementation of FPGA Based Quadcopter

Predictive Landing Guidance in Synthetic Vision Displays

Technology Considerations for Advanced Formation Flight Systems

AUTOMATIC FLIGHT CONTROL SYSTEM

Design of a Remote-Cockpit for small Aerospace Vehicles

Components Locked-On contains the following components:

Small Unmanned Aerial Vehicle Simulation Research

DCS FC3 - Sukhoi Su-27

WIND TUNNEL FREE-FLIGHT TEST FOR FLIGHT DYNAMICS AND CONTROL SYSTEM EXPERIMENTS

Operating Handbook. For. Gemini Autopilot

INSTRUCTION MANUAL CONTENTS

EXMITTER -- Professional Remote Control Products Expert

Development of Hybrid Flight Simulator with Multi Degree-of-Freedom Robot

If we want to show all the subsystems in the platform, we got the following detailed block diagrams of the platform.

AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS CHAPTER 4

Design Of An Autopilot For Small Unmanned Aerial Vehicles

Transcription:

Design of FBW Flight Control Systems for Modern Combat Aircraft Shyam Chetty Former Director, CSIR-NAL Bangalore 1 IIT Dharwad 2018 1

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

TEJAS 3 View - Geometry S = 38.4 m 2 b = 8.2 m AR = 1.751 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

Required Capabilities of Combat Aircraft in Attacking Air Targets 4

Required Capabilities of Combat Aircraft in Attacking Ground (Surface) Objects 5

Fully Loaded War Machine 6

With Laser Guided Bombs for Precision Ground Attack LGB LDP 7

CONTROL CONFIGURED VEHICLE (CCV) AERODYNAMICS CONTROL ACT * STRUCTURES PROPULSION * - ACTIVE CONTROL TECHNOLOGY 8

SIX Degrees of Freedom of Motion LATERAL YAW AXIAL ROLL VERTICAL PITCH 9

Aircraft Primary Controls Rudder ( Yaw ) Engine ( Thrust) Elevator ( Pitch ) Aileron ( Roll ) 10

Aircraft Control (Pitch) Elevators Video 11

Aircraft Control (Roll) Aileron Aileron Video 12

Aircraft Control (Yaw) Rudder Video 13

CONVENTIONAL AIRCRAFT 14

FLY-BY-WIRE FLIGHT CONTROL Computers + Sensors Actuators 15

A Tale of 4 Forces & 2 Ratios 16

How Drag is Reduced? 17

How is L/D & T/W increased 18

Flight Control Laws Brain 19

FBW Flight Control Hardware 20

DFCC 21

ACTUATORS 22

SENSORS 23

FCS Software Development 24

TEJAS FCS OFP SOFTWARE FUNCTIONS REAL TIME EXECUTIVE (SYNCHRONIZATION, SCHEDULING) 25

TEJAS IFCS Test Facilities 26

Control Law Schematic Glimpses into the exciting world of modern aircraft design 27

Human Pilot Modeling & Pilot- Aircraft Coupling Glimpses into the exciting world of modern aircraft design 28

Control Law Block Schematic Glimpses into the exciting world of modern aircraft design 29

Cockpit Controls HOTAS Hands On Throttle & Stick (30 to 40 functions being controlled) 38

HOTAS Stick Grip 39

HOTAS Throttle Grip Glimpses into the exciting world of modern aircraft design 40

THROTTLE Grip Controls 41

Tejas Cockpit aircraft Ergonomics Glass Cockpit Tejas (TD1, TD2 & PV1) Tejas (PV2) 42

TEJAS Cockpit Glass Displays Cockpit 43

HUD Head Landing Up display Configuration (HUD) 44

Helmet Mounted Display Helmet Mounted Display 45

Man-Machine Interaction 46

Development of Multi Function Autopilot

Development of Multi Function Autopilot

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

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

Flight Director 37

H / V NAV Mode Selection 31

Autopilot Mode / State Transitions

The CLAW Design Cycle 48

SIMULATION PLATFORMS Engineer In Loop Pilot In Loop Inflight Simulators 49

Iron Bird FCS Test Rig 50

Iron Bird Facility 51

Structural Coupling Rig 52

Airframe Structural Modes 53

Test & Integration Facilities 54

TEJAS Lightning Tests 55

Work Centers of LCA Programme 56

Industry Participation in LCA Programme 57

58

Cold Weather Trials at -15 deg C at Leh 59

Amidst Majestic Himalayas Video 60

Hot Weather +45 deg. C Trials at Jaisalmer 61

Wake Clearance 62

Air to Air Refueling 63

??? IIT Dharwad 2018