Rapid Prototyping a Two Channel Autopilot for a Generic Aircraft
|
|
|
- Judith Reed
- 6 years ago
- Views:
Transcription
1 Rapid Prototyping a Two Channel Autopilot for a Generic Aircraft YOGANANDA JEPPU Head R&D Systems Moog India Technology Center MATLAB EXPO India 2014
2 The Team Atit Mishra Basavaraj M Chethan CU Chinmayi J Manjunatha L Rao Surya Karthik Vanishree Yogananda at flights 4 fantasy, forum mall MATLAB EXPO India
3 Agenda What are autopilots Design Process Aircraft Model, Trims and Envelope Control Design Mode Transition Logic Code and Test 2 Channel Operation Demo I am not here to praise Matlab but its users who have done so much with it MATLAB EXPO India
4 Take away How a small team has been able to design a full fledged two channel autopilot with all the modes in a time frame of 8 months How Matlab and Simulink and the user community has helped us achieve this task Some things we have given back to the community MATLAB EXPO India
5 Autopilots MATLAB EXPO India
6 Autopilot Autopilot system is a mechanical, electrical or hydraulic system used to guide an airplane with minimal or no assistance from the pilot. It also reduces the fuel consumption and increases flight safety. Flight Director is a navigational aid that is overlaid on the attitude indicator that shows the pilot of an aircraft the attitude required to follow a certain trajectory. MATLAB EXPO India
7 Autopilot overview MATLAB EXPO India
8 MSCP Mode Select Control Panel This is developed using Matlab UI and has a real time interface with the Simulink simulation. It has a record and playback capability for system tests MATLAB EXPO India
9 PFD Primary Flight Display This is developed using the simple plot program and runs in real time displaying the Simulink data MATLAB EXPO India
10 Autopilot Modes MATLAB EXPO India
11 Vertical Modes PAH mode This is the basic autopilot mode in vertical axis. This mode holds the current pitch angle. Altitude Hold mode This mode holds the aircraft at the current altitude reference. Speed Hold mode This mode maintains the present airspeed. Vertical Speed mode This mode is used to automatically maintain the aircraft at a selected vertical speed (climb rate) reference. Altitude Select mode This mode captures the Selected Altitude. The 3 phases are, Arming, Capture and Hold. MATLAB EXPO India
12 Lateral Modes RAH mode This is the basic autopilot mode in lateral axis. This mode holds the current roll angle of the aircraft. Heading Hold mode This mode is used to hold the heading of the aircraft. Heading Select mode This mode is used to turn towards the Selected Heading. MATLAB EXPO India
13 Navigational Modes Go-Around mode The Go-Around mode is used transition from an approach mode to a climb mode when a missed approach occurs. Navigation VOR - This is a type of short-range radio navigation system for aircraft which defines the radials in space for tracking. MATLAB EXPO India
14 Approach Modes Approach mode This mode is used to approach the runway. Glide-slope and Localizer modes assist in vertical and lateral guidance. MATLAB EXPO India
15 Autothrottle and Yaw Damper An autothrottle mode is available to ensure that the engine maintains the speed or vertical speed reference. The yaw damper mode is also available to damp out the Dutch roll oscillation in yaw and maintain a low value of sideslip angle. In the yaw damper mode the commands are given to the rudder. These modes can be engaged with the main autopilot being off MATLAB EXPO India
16 Design Process MATLAB EXPO India
17 Linear Models Requirements Code Linear Control Test Non Linear Shaping Flight Envelope Simulations Deploy and Test MATLAB EXPO India
18 Aircraft Model, Trim, Envelope Did you just trim my Aircraft Son? MATLAB EXPO India
19 Aircraft Model Airlib by Giampiero Campa MATLAB EXPO India
20 Aircraft Trim Equilibrium point is computed optimally for a specific velocity(mach) and Altitude Lift = Weight Thrust = Drag All rates and Accelerations = 0 MATLAB EXPO India
21 Flight Envelope Mach MATLAB EXPO India
22 Flight Envelope MATLAB EXPO India
23 The FDC Toolbox M.O. Rauw MATLAB EXPO India
24 Pitch Attitude Hold Continuous Control Model MATLAB EXPO India
25 Rapid Prototyping fminsearch() MATLAB EXPO India
26 Scheduled Gains MATLAB EXPO India
27 Validation of Schedule Gains Scheduled gains validated against 1200 models in the flight envelope MATLAB EXPO India
28 Digital PAH These models are the SDD Requirements from which the C code is hand coded. MATLAB EXPO India
29 Mode Transition Logic Mode Transition table indicates the possible transitions from any operational mode to another mode due to an event. Event can be a software trigger or button press from the pilot. Condition table indicates the conditions that must be TRUE for the respective transition to occur. Conditions are tabulated in a separate table. MATLAB EXPO India
30 Validated with Assertions Starting from a safe state the autopilot modes have to transition to a safe state. The correctness of the safe state is verified by reviews Violation of any assertion for all combination of states, triggers and conditions requires a redesign of that transition This amounts to 36,391,680 executions during the validation process. 2 days of weekend runs MATLAB EXPO India
31 Code and Random Test MATLAB EXPO India
32 C Code and Test Manual coding with the utility functions for the various blocks Build each block using the utility functions Test each block using the mex function Random sinusoidal waveforms for float signals and random toggles for Boolean signals used to test the C code with the Simulink models Overnight runs cleared the code MATLAB EXPO India
33 UDP UDPIP by Giampiero Campa MATLAB EXPO India
34 UDP X-planes Simulink X-plane 10 UDP by Mohamed Abdelkader MATLAB EXPO India
35 Model in Loop Tests We have tried something new with the C code compiled as an exe and communicating with the Simulink model using UDP In a two channel operation we have two exe files communicating with each other and the expected result generated from the two channel stitched model MATLAB EXPO India
36 Error plots MATLAB EXPO India
37 Errors Moog does hand coding therefore there are going to be errors. Testing finds them! Lookup table data mismatch in the 4 th decimal place Logic errors between the model and code Input not connected properly in the model Initialization errors first frame Errors in mode transition One frame delays due to call order errors MATLAB EXPO India
38 Two Channel Operation MATLAB EXPO India
39 Cross Channel Sync Logic Channel A Increment Self Heart Beat HB Transmit Heart beat via CCDL HB Compute and hold offset when Both the channels are up Compute offset and compare with held offset Declare Sync if Offset = held offset Channel B Increment Self Heart Beat Declare Fail if offset!= Held offset MATLAB EXPO India
40 Demo MATLAB EXPO India
41 Google Maps plot_google_map - by Zohar Bar-Yehuda MATLAB EXPO India
42 Real time simulation Simulink Real Time Execution - by Guy Rouleau MATLAB EXPO India
43 Matlab UI Interface Simulink Signal Viewing using Event Listeners and a MATLAB UI - by Phil Goddard MATLAB EXPO India
44 GPS Navigation Black is desired track. Each leg is 100 Km Red is aircraft trajectory Latitude (Deg) Longitude (Deg) MATLAB EXPO India
45 GPS Navigation Latitude (Deg) Longitude (Deg) MATLAB EXPO India
46 Matlab Toolboxes We used these toolboxes for our design Matlab and Simulink Control System Toolbox Aerospace Blockset Real Time Coder MATLAB EXPO India
47 Our Contributions We have tried to give back to the Matlab community. It has made a moderate impact going by the download rate and comments MATLAB EXPO India
48 Safety Critical Blocks Safety Critical Control Elements Examples - by Chethan C U MATLAB EXPO India
49 Random Signal Generation Random Signal Generationby Chethan C U MATLAB EXPO India
50 Testing Safety Critical Systems Testing of Safety Critical Control Systems - by Yogananda Jeppu MATLAB EXPO India
51 Final Words The idea is to try to give all the information to help others to judge the value of your contribution; not just the information that leads to judgment in one particular direction or another. - Richard P. Feynman Finally - Thank you Mathworks for making this possible jyogananda@moog.com MATLAB EXPO India
52 Video 3 Mins. Questions? MATLAB EXPO India
Fokker 50 - Automatic Flight Control System
GENERAL The Automatic Flight Control System (AFCS) controls the aircraft around the pitch, roll, and yaw axes. The system consists of: Two Flight Directors (FD). Autopilot (AP). Flight Augmentation System
Digiflight II SERIES AUTOPILOTS
Operating Handbook For Digiflight II SERIES AUTOPILOTS TRUTRAK FLIGHT SYSTEMS 1500 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 Toll Free: 866-TRUTRAK 866-(878-8725) www.trutrakap.com
Operating Handbook For FD PILOT SERIES AUTOPILOTS
Operating Handbook For FD PILOT SERIES AUTOPILOTS TRUTRAK FLIGHT SYSTEMS 1500 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 Toll Free: 866-TRUTRAK 866-(878-8725) www.trutrakap.com
Classical Control Based Autopilot Design Using PC/104
Classical Control Based Autopilot Design Using PC/104 Mohammed A. Elsadig, Alneelain University, Dr. Mohammed A. Hussien, Alneelain University. Abstract Many recent papers have been written in unmanned
Small Unmanned Aerial Vehicle Simulation Research
International Conference on Education, Management and Computer Science (ICEMC 2016) Small Unmanned Aerial Vehicle Simulation Research Shaojia Ju1, a and Min Ji1, b 1 Xijing University, Shaanxi Xi'an, 710123,
EMBRAER 135/145 Autopilot
EMBRAER 135/145 Autopilot GENERAL The Primus 1000 (P-1000) Automatic Flight Control System (AFCS) is a fully integrated, fail passive three-axis flight control system which incorporates lateral and vertical
SECTION 2-19 AUTOPILOT
AIRPLANE SECTION 2-19 Block General...2-19-05...01 Automatic Flight Control System...2-19-05...02 Flight Guidance System...2-19-05...04 Flight Director...2-19-05...04 Autopilot...2-19-05...04 Flight Director
17 Wellington Business Park Crowthorne Berkshire RG45 6LS England. Tel: +44 (0)
17 Wellington Business Park Crowthorne Berkshire RG45 6LS England Tel: +44 (0) 1344 234047 www.flightdatapeople.com Information Sheet www.flightdatapeople.com Commercial in Confidence Hosted Flight Data
Dash8-200/300 - Automatic Flight AUTOMATIC FLIGHT CONTROLS AND INDICATORS. Page 1
AUTOMATIC FLIGHT CONTROLS AND INDICATORS FLIGHT GUIDANCE MODE SELECTORS (alternate action) - Engages flight director modes of operation. - Flight director command bars display lateral and/or vertical guidance
Modeling and simulation of naval radar scenarios using imported target data in Adapt MFR and v software release notes
Modeling and simulation of naval radar scenarios using imported target data in Adapt MFR and v3.2.12 software release notes Prepared by: B. Brinson and J. Chamberland C-CORE, 4043 Carling Ave., Suite 202,
CHAPTER 5 AUTOMATIC LANDING SYSTEM
117 CHAPTER 5 AUTOMATIC LANDING SYSTEM 51 INTRODUCTION The ultimate aim of both military and commercial aviation is allweather operation To achieve this goal, it should be possible to land the aircraft
Hardware-in-the-Loop Simulation for a Small Unmanned Aerial Vehicle A. Shawky *, A. Bayoumy Aly, A. Nashar, and M. Elsayed
16 th International Conference on AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 May 26-28, 2015, E-Mail: asat@mtc.edu.eg Military Technical College, Kobry Elkobbah, Cairo, Egypt Tel : +(202) 24025292
Digiflight II SERIES AUTOPILOTS
Operating Handbook For Digiflight II SERIES AUTOPILOTS TRUTRAK FLIGHT SYSTEMS 1500 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 Toll Free: 866-TRUTRAK 866-(878-8725) www.trutrakap.com
Post-Installation Checkout All GRT EFIS Models
GRT Autopilot Post-Installation Checkout All GRT EFIS Models April 2011 Grand Rapids Technologies, Inc. 3133 Madison Avenue SE Wyoming MI 49548 616-245-7700 www.grtavionics.com Intentionally Left Blank
Desktop real time flight simulator for control design
Desktop real time flight simulator for control design By T Vijeesh, Technical Officer, FMCD, CSIR-NAL, Bangalore C Kamali, Scientist, FMCD, CSIR-NAL, Bangalore Prem Kumar B, Project Assistant,,FMCD, CSIR-NAL,
Design of FBW Flight Control Systems for Modern Combat Aircraft Shyam Chetty Former Director, CSIR-NAL Bangalore
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
FlyRealHUDs Very Brief Helo User s Manual
FlyRealHUDs Very Brief Helo User s Manual 1 1.0 Welcome! Congratulations. You are about to become one of the elite pilots who have mastered the fine art of flying the most advanced piece of avionics in
AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS CHAPTER 4
TABLE OF CONTENTS CHAPTER 4 Page TABLE OF CONTENTS DESCRIPTION General Guidance Panel Autopilot System Autopilot Yaw Damper Autopilot Engage Autopilot Disengage PFD Annunciation Flight Director (FD) Flight
Flight Detector Indicator
Flight Detector Indicator Part No: 777-1224-003 Components Maintenance Manual No: 34-25-12 By Soumyadeep Das Raj shekhar Chatterjee Purpose of equipment: The flight detector indicator (FDI) is a part of
Flight control system for a reusable rocket booster on the return flight through the atmosphere
Flight control system for a reusable rocket booster on the return flight through the atmosphere Aaron Buysse 1, Willem Herman Steyn (M2) 1, Adriaan Schutte 2 1 Stellenbosch University Banghoek Rd, Stellenbosch
Multi-Axis Pilot Modeling
Multi-Axis Pilot Modeling Models and Methods for Wake Vortex Encounter Simulations Technical University of Berlin Berlin, Germany June 1-2, 2010 Ronald A. Hess Dept. of Mechanical and Aerospace Engineering
FLCS V2.1. AHRS, Autopilot, Gyro Stabilized Gimbals Control, Ground Control Station
AHRS, Autopilot, Gyro Stabilized Gimbals Control, Ground Control Station The platform provides a high performance basis for electromechanical system control. Originally designed for autonomous aerial vehicle
Operating Handbook. For. Gemini Autopilot
Operating Handbook For Gemini Autopilot TRUTRAK FLIGHT SYSTEMS 1488 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 www.trutrakap.com Table of Contents 1. Revisions... 5 2.
Operating Handbook. For. Gemini Autopilot
Operating Handbook For Gemini Autopilot TRUTRAK FLIGHT SYSTEMS 1488 S. Old Missouri Road Springdale, AR 72764 Ph. 479-751-0250 Fax 479-751-3397 www.trutrakap.com Table of Contents 1. Revisions... 5 2.
MGL Avionics. iefis. Integrated Autopilot. User and installation manual. Manual dated 14 November Page 1
MGL Avionics iefis Integrated Autopilot User and installation manual Manual dated 14 November 2014 Page 1 Table of Contents General...4 Autopilot abilities...4 External autopilot systems...4 Internal autopilot
Flight Dynamics AE426
KING FAHD UNIVERSITY Department of Aerospace Engineering AE426: Flight Dynamics Instructor Dr. Ayman Hamdy Kassem What is flight dynamics? Is the study of aircraft motion and its characteristics. Is it
Matlab/Simulink Tools for Teaching Flight Control Conceptual Design: An Integrated Approach
Matlab/Simulink Tools for Teaching Flight Control Conceptual Design: An Integrated Approach Hanyo Vera Anders Tomas Melin Arthur Rizzi The Royal Institute of Technology, Sweden. 1 Presentation Outline
A Mini UAV for security environmental monitoring and surveillance: telemetry data analysis
A Mini UAV for security environmental monitoring and surveillance: telemetry data analysis G. Belloni 2,3, M. Feroli 3, A. Ficola 1, S. Pagnottelli 1,3, P. Valigi 2 1 Department of Electronic and Information
This page is intentionally blank. GARMIN G1000 SYNTHETIC VISION AND PATHWAYS OPTION Rev 1 Page 2 of 27
This page is intentionally blank. 190-00492-15 Rev 1 Page 2 of 27 Revision Number Page Number(s) LOG OF REVISIONS Description FAA Approved Date of Approval 1 All Initial Release See Page 1 See Page 1 190-00492-15
Aerospace Sensor Suite
Aerospace Sensor Suite ECE 1778 Creative Applications for Mobile Devices Final Report prepared for Dr. Jonathon Rose April 12 th 2011 Word count: 2351 + 490 (Apper Context) Jin Hyouk (Paul) Choi: 998495640
GPS Flight Control in UAV Operations
1 Antenna, GPS Flight Control in UAV Operations CHANGDON KEE, AM CHO, JIHOON KIM, HEEKWON NO SEOUL NATIONAL UNIVERSITY GPS provides position and velocity measurements, from which attitude information can
SkyView. Autopilot In-Flight Tuning Guide. This product is not approved for installation in type certificated aircraft
SkyView Autopilot In-Flight Tuning Guide This product is not approved for installation in type certificated aircraft Document 102064-000, Revision B For use with firmware version 10.0 March, 2014 Copyright
VOR/DME APPROACH WITH A320
1. Introduction VOR/DME APPROACH WITH A320 This documentation presents an example of a VOR/DME approach performed with an Airbus 320 at LFRS runway 21. This type of approach is a non-precision approach
Modeling and Simulation Made Easy with Simulink Carlos Osorio Principal Application Engineer MathWorks Natick, MA
Modeling and Simulation Made Easy with Simulink Carlos Osorio Principal Application Engineer MathWorks Natick, MA 2013 The MathWorks, Inc. 1 Questions covered in this presentation 1. Why do we do modeling
Safety Enhancement SE (R&D) ASA - Research Attitude and Energy State Awareness Technologies
Safety Enhancement SE 207.1 (R&D) ASA - Research Attitude and Energy State Awareness Technologies Safety Enhancement Action: Statement of Work: Aviation community (government, industry, and academia) performs
AUTOMATIC FLIGHT CONTROL SYSTEM TABLE OF CONTENTS CHAPTER 4
TABLE OF CONTENTS CHAPTER 4 Page TABLE OF CONTENTS DESCRIPTION General Guidance Panel Autopilot System Autopilot Yaw Damper Autopilot Engage Autopilot Disengage PFD Annunciation Flight Director (FD) Flight
NAVIGATION INSTRUMENTS - BASICS
NAVIGATION INSTRUMENTS - BASICS 1. Introduction Several radio-navigation instruments equip the different airplanes available in our flight simulators software. The type of instrument that can be found
Module 2: Lecture 4 Flight Control System
26 Guidance of Missiles/NPTEL/2012/D.Ghose Module 2: Lecture 4 Flight Control System eywords. Roll, Pitch, Yaw, Lateral Autopilot, Roll Autopilot, Gain Scheduling 3.2 Flight Control System The flight control
Page Chg
Page Chg Cover...0 Page #...2 TOC-1...2 TOC-2..2 1-1 2 1-2.2 1-3.2 1-4...2 1-5...2 1-6. 2 1-7. 2 1-8. 2 1-9. 2 1-10...2 1-11..2 1-12..2 1-13..2 1-14..2 1-15..2 1-16..2 1-17..2 1-18...2 2-1.0 2-2.0 2-3.2
BLACKBOARD ARCHITECTURE FOR AN UNMANNED AERIAL VEHICLE CONTROLLER USING FUZZY INFERENCE SYSTEMS SWETHA PANDHITI
BLACKBOARD ARCHITECTURE FOR AN UNMANNED AERIAL VEHICLE CONTROLLER USING FUZZY INFERENCE SYSTEMS by SWETHA PANDHITI (Under the Direction of Walter D. Potter) ABSTRACT The objective of this research is to
Design of Missile Two-Loop Auto-Pilot Pitch Using Root Locus
International Journal Of Advances in Engineering and Management (IJAEM) Page 141 Volume 1, Issue 5, November - 214. Design of Missile Two-Loop Auto-Pilot Pitch Using Root Locus 1 Rami Ali Abdalla, 2 Muawia
Page Chg
Page Chg Cover...0 Page #...1 TOC-1...1 TOC-2..1 1-1.1 1-2.1 1-3.1 1-4...0 1-5...1 1-6. 1 1-7. 1 1-8. 1 1-9. 1 1-10...1 1-11..1 1-12..1 1-13..1 1-14..1 2-1.0 2-2.0 2-3.1 Page Chg 2-4.0 3-1.0 3-2.0 3-3.0
What's New in MATLAB and Simulink for Signal Processing? Daniel Aronsson, Application Engineer
What's New in MATLAB and Simulink for Signal Processing? Daniel Aronsson, Application Engineer 2014 The MathWorks, Inc. 1 Signal Processing 2 Harmonic and Intermodulation Distortion Measurement Industry-standard
UAV: Design to Flight Report
UAV: Design to Flight Report Team Members Abhishek Verma, Bin Li, Monique Hladun, Topher Sikorra, and Julio Varesio. Introduction In the start of the course we were to design a situation for our UAV's
Page Chg
Page Chg Cover...0 Page #...4 TOC-1...3 TOC-2..3 1-1 2 1-2.3 1-3.3 1-4...3 1-5...3 1-6. 3 1-7. 3 1-8. 4 1-9. 4 1-10...3 1-11..4 1-12..4 1-13..3 1-14..3 1-15..3 1-16..3 1-17..3 1-18...3 1-19..3 2-1.0 2-2.0
MGL Avionics EFIS. Integrated Autopilot. User and installation manual. Manual dated 24 May 2010
MGL Avionics EFIS Integrated Autopilot User and installation manual Manual dated 24 May 2010 This manual supersedes all previous versions and is applicable for current EFIS firmware versions Page 1 Table
Cockpit Visualization of Curved Approaches based on GBAS
www.dlr.de Chart 1 Cockpit Visualization of Curved Approaches based on GBAS R. Geister, T. Dautermann, V. Mollwitz, C. Hanses, H. Becker German Aerospace Center e.v., Institute of Flight Guidance www.dlr.de
412 th Test Wing. War-Winning Capabilities On Time, On Cost. Lessons Learned While Giving Unaugmented Airplanes to Augmentation-Dependent Pilots
412 th Test Wing War-Winning Capabilities On Time, On Cost Lessons Learned While Giving Unaugmented Airplanes to Augmentation-Dependent Pilots 20 Nov 2012 Bill Gray USAF TPS/CP Phone: 661-277-2761 Approved
HAZARD AVOIDANCE. Displaying traffic on the Navigation Map. Displaying traffic information (PFD Inset Map):
HAZARD AVOIDANCE Displaying traffic on the Navigation Map 1) Ensure that the TAS system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is
If we want to show all the subsystems in the platform, we got the following detailed block diagrams of the platform.
Design and Development of a Networked Control System Platform for Unmanned Aerial Vehicles 1 Yücel Taş, 2 Aydın Yeşildirek, 3 Ahmet Sertbaş 1 Istanbul University, Computer Engineering Dept., Istanbul,
Page Chg
Page Chg Cover...0 Page #...1 TOC-1...1 TOC-2...1 1-1.1 1-2.0 1-3.1 1-4...1 1-5...1 1-6. 1 1-7. 1 1-8. 1 1-9. 1 1-10...1 1-11..1 1-12..1 1-13..2 1-14..1 1-15..1 1-16..1 1-17..1 1-18..1 2-1.0 2-2.0 Page
A New Perspective to Altitude Acquire-and- Hold for Fixed Wing UAVs
Student Research Paper Conference Vol-1, No-1, Aug 2014 A New Perspective to Altitude Acquire-and- Hold for Fixed Wing UAVs Mansoor Ahsan Avionics Department, CAE NUST Risalpur, Pakistan mahsan@cae.nust.edu.pk
GPS System Design and Control Modeling. Chua Shyan Jin, Ronald. Assoc. Prof Gerard Leng. Aeronautical Engineering Group, NUS
GPS System Design and Control Modeling Chua Shyan Jin, Ronald Assoc. Prof Gerard Leng Aeronautical Engineering Group, NUS Abstract A GPS system for the autonomous navigation and surveillance of an airship
Design of a Flight Stabilizer System and Automatic Control Using HIL Test Platform
Design of a Flight Stabilizer System and Automatic Control Using HIL Test Platform Şeyma Akyürek, Gizem Sezin Özden, Emre Atlas, and Coşku Kasnakoğlu Electrical & Electronics Engineering, TOBB University
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR. Trio Pro Pilot Autopilot
Page 1 480 Ruddiman Drive TRIO AP Flight Manual Supplement North Muskegon, MI 49445 L-1006-01 Rev D FOR Trio Pro Pilot Autopilot ON Cessna 172, 175, 177, 180, 182, 185 and Piper PA28 Aircraft Document
AUTOMATIC FLIGHT CONTROL SYSTEM
TRIDEN AUTOMATIC FLIGHT CONTROL SYSTEM PILOT S OPERATING HANDBOOK 68S1135 Rev B 02-05-03 FACTORY SERVICE CENTERS Century Flight Systems, Inc. has established Factory owned and operated Customer Service
AIRCRAFT AVIONIC SYSTEMS
AIRCRAFT AVIONIC SYSTEMS B-777 cockpit Package C:\Documents and ettings\administrato Course Outline Radio wave propagation Aircraft Navigation Systems - Very High Omni-range (VOR) system - Instrument Landing
Table of Contents. Introduction 3. Pictorials of the 40 and 50 Systems 4. List of Applicable Acronyms 6
Table of Contents Introduction 3 Pictorials of the 40 and 50 Systems 4 List of Applicable Acronyms 6 System 40 Modes of Operation 7 System 40 Functional Preflight Procedures 10 System 40 In Flight Procedures
Dash8 - Q400 - Autoflight
12.3.1 Introduction The Automatic Flight Control System (AFCS), provides fail-safe operation of flight director guidance, autopilot, yaw damper and automatic pitch trim functions. 12.3.2 General The Automatic
GRT Autopilot User Guide. All GRT EFIS Systems
All GRT EFIS Systems Revision A 22-May-2014 Copyright 2014 3133 Madison Ave. SE Wyoming, MI 49548 (616) 245-7700 www.grtavionics.com Revision Notes Revision Date Change Description A 22-May-2014 Complete
and using the step routine on the closed loop system shows the step response to be less than the maximum allowed 20%.
Phase (deg); Magnitude (db) 385 Bode Diagrams 8 Gm = Inf, Pm=59.479 deg. (at 62.445 rad/sec) 6 4 2-2 -4-6 -8-1 -12-14 -16-18 1-1 1 1 1 1 2 1 3 and using the step routine on the closed loop system shows
New functions and changes summary
New functions and changes summary A comparison of PitLab & Zbig FPV System versions 2.50 and 2.40 Table of Contents New features...2 OSD and autopilot...2 Navigation modes...2 Routes...2 Takeoff...2 Automatic
STC FLIGHT FUNCTIONAL TEST
GDC31 Roll Steering Converter 1049-2080-02 REV A 2004, DAC International All Rights Reserved. 6702 McNeil Drive Austin, Texas 78729 (512) 331-5323 Phone (512) 331-4516 Fax Page 1 of 14 Record of Revisions
NAVIGATION AND PITOT-STATIC SYSTEMS
NAVIGATION AND PITOT-STATIC SYSTEMS. GENERAL This chapter describes the navigation systems, units, and components which provide airplane navigational information. Included are pitot-static, gyros, compass,
Automatic Recovery and Autonomous Navigation of Disabled Aircraft After Control Surface Actuator Jam
Automatic Recovery and Autonomous Navigation of Disabled Aircraft After Control Surface Actuator Jam Coşku Kasnakoğlu, Ünver Kaynak TOBB University of Economics and Technology, Ankara, 656, Turkey Loss
FLIGHT DATA MONITORING
FLIGHT DATA MONITORING RECORD REPLAY REVIEW FLIGHT DATA MONITORING FLIGHT TRAINING INCIDENT INVESTIGATION APPAREO S TURN-KEY FLIGHT DATA MONITORING SUITE When it comes to flight safety, there s nothing
Recent Progress in the Development of On-Board Electronics for Micro Air Vehicles
Recent Progress in the Development of On-Board Electronics for Micro Air Vehicles Jason Plew Jason Grzywna M. C. Nechyba Jason@mil.ufl.edu number9@mil.ufl.edu Nechyba@mil.ufl.edu Machine Intelligence Lab
STUDY OF FIXED WING AIRCRAFT DYNAMICS USING SYSTEM IDENTIFICATION APPROACH
STUDY OF FIXED WING AIRCRAFT DYNAMICS USING SYSTEM IDENTIFICATION APPROACH A.Kaviyarasu 1, Dr.A.Saravan Kumar 2 1,2 Department of Aerospace Engineering, Madras Institute of Technology, Anna University,
Various levels of Simulation for Slybird MAV using Model Based Design
Various levels of Simulation for Slybird MAV using Model Based Design Kamali C Shikha Jain Vijeesh T Sujeendra MR Sharath R Motivation In order to design robust and reliable flight guidance and control
Tiny Flight Tracker & Viewer Manual
Tiny Flight Tracker & Viewer Manual Version 3.xx Note: Program version number that appears in the pictures of this document may not reflect the latest available release. Tiny Flight Tracker & Viewer v3.xx
Instrument Flight Procedures - Glass Cockpits
Instrument Flight Procedures - Glass Cockpits The concepts contained here are general in nature and can be used by all however, they are targeted toward glass cockpits and, more specifically, integrated
The J2 Universal Tool-Kit - Linear Analysis with J2 Classical
The J2 Universal Tool-Kit - Linear Analysis with J2 Classical AIRCRAFT MODELLING AND PERFORMANCE PREDICTION SOFTWARE Key Aspects INTRODUCTION Why Linear Analysis? J2 Classical J2 CLASSICAL AS PART OF THE
Detrum MSR66A Receiver
Motion RC User Guide for the Detrum MSR66A Receiver Version 1.0 Contents Review the Receiver s Features... 1 Review the Receiver s Ports and Connection Orientation... 2 Bind the Receiver to a Transmitter
How to Intercept a Radial Outbound
How to Intercept a Radial Outbound by Greg Whiley Another practical publication from Aussie Star Flight Simulation How to intercepting a radial outbound 1 Greg Whiley Aussie Star Flight Simulation How
Flight Simulation for Tomorrow's Aviation
Flight Simulation for Tomorrow's Aviation Dr.Umut Durak DLR Institute of Flight Systems ASIM STS/GMMS 2016 Workshop Lippstadt, 10.3. - 11.3.2016 Flying is safer then ever! Ref: Boeing, Statistical Summary
Steering a Flat Circular Parachute They Said It Couldn t Be Done
17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 19-22 May 2003, Monterey, California AIAA 2003-2101 Steering a Flat Circular Parachute They Said It Couldn t Be Done S. Dellicker
SD3-60 AIRCRAFT MAINTENANCE MANUAL
AMM 24.0.0.0FLIGHT DIRECTOR SYSTEM - DESCRIPTION & OPERATION 1. Description A. General Refer to Figure 1. Identical, left and right, systems are installed (one for each pilot); each provides information
Neural Flight Control Autopilot System. Qiuxia Liang Supervisor: dr. drs. Leon. J. M. Rothkrantz ir. Patrick. A. M. Ehlert
Neural Flight Control Autopilot System Qiuxia Liang Supervisor: dr. drs. Leon. J. M. Rothkrantz ir. Patrick. A. M. Ehlert Introduction System Design Implementation Testing and Improvements Conclusions
GX Pilot Series Autopilots
GX Pilot Series Autopilots Installation/User Manual TRUTRAK FLIGHT SYSTEMS 1500 S. Old Missouri Road Springdale, AR 72764 POSTAL SERVICE ADDRESS P.O. Box 189 Springdale, AR 72765-0189 Ph: 479-751-0250
Module 13 Aircraft Aerodynamics, Structures and Systems
13.1 Theory of Flight (a) Aeroplane Aerodynamics and Flight Controls Operation and effect of: roll control: ailerons and spoilers, pitch control: elevators, stabilators, variable incidence stabilisers
The Pennsylvania State University. The Graduate School. College of Engineering
The Pennsylvania State University The Graduate School College of Engineering INTEGRATED FLIGHT CONTROL DESIGN AND HANDLING QUALITIES ANALYSIS FOR A TILTROTOR AIRCRAFT A Thesis in Aerospace Engineering
Design and Simulation of Flight Path Control Systems for CHARLIE Aircraft
IOSR Journal of Electronics and Communication Engineering (IOSR-JECE) e-issn: 2278-2834,p- ISSN: 2278-8735.Volume 11, Issue 3, Ver. IV (May-Jun.216), PP 35-44 www.iosrjournals.org Design and Simulation
Long Range Wireless OSD 5.8G FPV Transmitter
Long Range Wireless OSD 5.8G FPV Transmitter Built-in 10 Axis AHRS + MAVLINK + 600mW Support all flight controller and GPS 1 / 14 User's Guide Catalogue Product Instruction 3 Features 3 Specifications.4
International Journal of Advance Engineering and Research Development. Aircraft Pitch Control System Using LQR and Fuzzy Logic Controller
Scientific Journal of Impact Factor (SJIF): 4.14 International Journal of Advance Engineering and Research Development Volume 3,Issue 5,May -216 e-issn : 2348-447 p-issn : 2348-646 Aircraft Pitch Control
Improving Lunar Return Entry Footprints Using Enhanced Skip Trajectory Guidance
Improving Lunar Return Entry Footprints Using Enhanced Skip Trajectory Guidance Z. R. Putnam * and R. D. Braun Georgia Institute of Technology, Atlanta, GA, and S. H. Bairstow and G. H. Barton Charles
Page 1/10 Digilent Analog Discovery (DAD) Tutorial 6-Aug-15. Figure 2: DAD pin configuration
Page 1/10 Digilent Analog Discovery (DAD) Tutorial 6-Aug-15 INTRODUCTION The Diligent Analog Discovery (DAD) allows you to design and test both analog and digital circuits. It can produce, measure and
Design of Accurate Navigation System by Integrating INS and GPS using Extended Kalman Filter
Design of Accurate Navigation System by Integrating INS and GPS using Extended Kalman Filter Santhosh Kumar S. A 1, 1 M.Tech student, Digital Electronics and Communication Systems, PES institute of technology,
302 VIBROENGINEERING. JOURNAL OF VIBROENGINEERING. MARCH VOLUME 15, ISSUE 1. ISSN
949. A distributed and low-order GPS/SINS algorithm of flight parameters estimation for unmanned vehicle Jiandong Guo, Pinqi Xia, Yanguo Song Jiandong Guo 1, Pinqi Xia 2, Yanguo Song 3 College of Aerospace
OughtToPilot. Project Report of Submission PC128 to 2008 Propeller Design Contest. Jason Edelberg
OughtToPilot Project Report of Submission PC128 to 2008 Propeller Design Contest Jason Edelberg Table of Contents Project Number.. 3 Project Description.. 4 Schematic 5 Source Code. Attached Separately
Implementation of Nonlinear Reconfigurable Controllers for Autonomous Unmanned Vehicles
Implementation of Nonlinear Reconfigurable Controllers for Autonomous Unmanned Vehicles Dere Schmitz Vijayaumar Janardhan S. N. Balarishnan Department of Mechanical and Aerospace engineering and Engineering
PC-Based Human-In-the-Loop Simulation for Flight
Applied Mechanics and Materials Vols. 0-2 (2008) pp 476-482 Online available since 2007/Dec/06 at www.scientific.net (2008) Trans Tech Publications, Switzerland doi:0.4028/www.scientific.net/amm.0-2.476
Project Number: 13231
Multidisciplinary Senior Design Conference Kate Gleason College of Engineering Rochester Institute of Technology Rochester, New York 14623 Project Number: 13231 UAV GROUND-STATION AND SEEDED FAULT DETECTION
SMART BIRD TEAM UAS JOURNAL PAPER
SMART BIRD TEAM UAS JOURNAL PAPER 2010 AUVSI STUDENT COMPETITION MARYLAND ECOLE POLYTECHNIQUE DE MONTREAL Summary 1 Introduction... 4 2 Requirements of the competition... 4 3 System Design... 5 3.1 Design
FLIGHTZOOMER 2.0 NEW FEATURES
FLIGHTZOOMER 2.0 NEW FEATURES 1 1 Contents 2 Disclaimer... 3 3 Overview... 4 3.1 Document scope... 4 3.2 Project history... 4 3.3 FlightZoomer in a nutshell... 5 3.3.1 High level requirements... 5 3.3.2
Flight-dynamics Simulation Tools
Flight-dynamics Simulation Tools 2 nd ESA Workshop on Astrodynamics Tools and Techniques ESTEC, September 13-15, 2004 Erwin Mooij Introduction (1) Areas of interest (not complete): Load analysis and impact-area
UNDERSTANDING LTE WITH MATLAB
UNDERSTANDING LTE WITH MATLAB FROM MATHEMATICAL MODELING TO SIMULATION AND PROTOTYPING Dr Houman Zarrinkoub MathWorks, Massachusetts, USA WILEY Contents Preface List of Abbreviations 1 Introduction 1.1
Development of Hybrid Flight Simulator with Multi Degree-of-Freedom Robot
Development of Hybrid Flight Simulator with Multi Degree-of-Freedom Robot Kakizaki Kohei, Nakajima Ryota, Tsukabe Naoki Department of Aerospace Engineering Department of Mechanical System Design Engineering
KAP 140 Two Axis with Altitude Preselect Operation
Two Axis/Altitude reselect Operations K 0 Two Axis with Altitude reselect Operation The K 0 is a digital, panel-mounted autopilot system for light aircraft. 7 8 K 0 D AV V AT D Two-axis w/altitude reelect
ELITE Operator s Manual
ELITE Jet v8 ELITE Operator s Manual The aircraft simulated by ELITE Jet represents the well known civil airliner MD-81. The instrumentation of the cockpit represents all standard instruments. Only the
Intermediate Lateral Autopilots (I) Yaw orientation control
Intermediate Lateral Autopilots (I) Yaw orientation control Yaw orientation autopilot Lateral autopilot for yaw maneuver Designed to have the aircraft follow the pilot's yaw rate command or hold the aircraft