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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
985605
Design and Implementation of a State-Estimation System Utilizing a Low-Cost Distributed Sensor Array
 
985540
Development of a Cockpit Situation Display for Free-Flight
 
985543
Simultaneous Design of Cockpit Display of Traffic Information and Air Traffic Management Procedures
 
975626
FLASH Flight Control Systems
 
975631
SOFIA Science Utilization: The US Science Instrument Program
 
965534
A Methodology for Identifying Information Requirements and Interaction Issues for an HSCT Autoflight System
 
965551
Taxiway Navigation and Situation Awareness (T-NASA) System: Problem, Design Philosophy, and Description of an Integrated Display Suite for Low-Visibility Airport Surface Operations
 
952024
A Perspective on Commercial and Military Avionics
 
952036
An Examination of Aircraft Aerodynamic Estimation Using Neural Networks
 
951994
DC-X Hydraulic Flight Control System
 
951992
Digital Flight Control Actuation
 
952044
FLASH Fly-By-Light Flight Control Systems Development and Demonstrations
 
952042
Fly-by-Light Advanced Systems Hardware (FLASH) Program Society of Automotive Engineers Aerotech Meeting
 
952028
Mixed Voltage, Microprocessor Based Avionic Systems
 
952029
Off-The-Shelf Multi-Language Tool Support for Embedded Intel386™ EX Processor
 
952043
The Aircraft Optical Cable Plant Program: The Physical Layer for Fly-By-Light Control Networks
 
952046
The Development of a Helicopter Visually-Coupled System Research Facility
 
951446
A Smart Actuation System for High Performance Flight Control Systems
 
951429
Exploratory Applications of New Aerodynamic Control Devices
 
942554
A Millimeter Wave, Wireless, LAN for Use Inside an Aircraft
 
942169
Real-Time Executive Monitor (RTEM)
 
941173
Flight Control Maintenance Diagnostic System (FCMDS) Field Testing Results and Future Plans
 
940001
Flight Path Control for the Approach and Landing of the Quiet STOL Experimental Aircraft ASKA
 
932521
A Market Perspective on FANS
 
932630
Diagnostics for Electrohydraulic Primary Flight Control Servoactuators
 
931600
1553 RT Mechanizations for Data Sample Consistency and Multi-Message Transfers
 
931388
A Detailed Power Inverter Design for a 250 kW Switched Reluctance Aircraft Engine Starter/Generator
 
931590
A Single-Supply, Monolithic, MIL-STD-1553 Transceiver Implemented in BiCMOS Wafer Fabrication Technology
 
931400
Aircraft Landing Gear Dynamics Present and Future
 
931598
Changing the Utility Subsystem Paradigm
 
931389
Detailed Design of a 250-kW Switched Reluctance Starter/Generator for an Aircraft Engine
 
931591
Development Methodology for Contemporary Avionics Systems
 
931594
Experiences in Validating MIL-STD-1553 Remote Terminals
 
931439
Fiber Optic Hardware for Transport Aircraft
 
931597
High Speed Databus Evaluation: Further Work
 
931415
Integrated IR Sensors
 
931417
Integrated Test System Single Point Control of Aircraft Checkout
 
931596
JIAWG Compatible Development Boards for the i960
 
931592
MIL-STD-1553 Remote Terminal Design Using ASIC Megacell Technology
 
931416
Modular Avionics: Taking Today's Aircraft into Tomorrow
 
931593
Modular Electro-Optic Data Bus Coupler
 
931406
Power System Characteristics for More Electric Aircraft
 
931595
STANAG 3910 - The Data Bus for the Next Generation of European Avionics Systems
 
931599
The Space Avionics Architecture Standard Tailored to the Common Lunar Lander Conceptual Design
 
921471
Analysis and Design of Microstrip Antennas for Aircraft Applications
 
921520
Autoflight and Powerplant Integration of Last Generation Commuter Aircraft
 
921964
Recent Advances in No-Break Power Transfer (NBPT)
 
921967
Situation vs. Command Guidance Symbology for Hybrid Landing Systems Applications
 
921966
Solid-State Power Controllers Meet System Demands
 
922028
YF-23A HYDRAULIC MANAGEMENT SYSTEM
 
920967
The Integral Starter/Generator Development Progress
 
920968
The Integrated Actuation Package Approach to Primary Flight Control
 
912148
Controls for Agility Research in the NASA High-Alpha Technology Program
 
912080
Development of the DDV Actuation System on the IDF Aircraft
 
912107
ELS Pilot Evaluation
 
912111
ELS for the A340
 
912050
Electric Power Generating System for the Boeing 777 Airplane
 
912036
Functional Mock-Up Tests for Flight Control System of the NAL QSTOL Research Aircraft ‘ASKA’
 
912112
Integrating an ELS into an Existing Aircraft Design
 
912108
Multidimensional ELS User Interface
 
912144
On Upsets of Analog Portions of Digital Flight Control Systems Due to Electromagnetic Interference
 
912005
Results and Lessons Learned from the STOL & Maneuver Demonstration Program
 
912109
The Document Revision Process for the Electronic Library System
 
911413
Flight Firing Operations on the ITALSAT F1 R-4D-11 Thruster
 
911008
Automatic Flight Control System Honeywell SPZ-7600 (AFCS) for Search and Rescue Helicopters
 
911200
Electric Brake System Modeling and Simulation
 
911112
Flight Control Actuation System for the B-2 Advanced Technology Bomber
 
911197
Flight Deck Automation: Strategies for Use Now and in the Future
 
911107
Testing of the V-22 Flight Control System
 
902341
Implementation of New Technology - A Boeing Perspective
 
902016
A Thinner Flight Control Actuator
 
902024
Advanced Technology Servoactuator
 
901957
Airline Data Link Automation Progress and Issues
 
901828
Alaska Airlines Experience with the HGS-1000 Head Up Guidance System
 
901900
All Digital Electrohydrostatic Servoactuator
 
901803
Application of a Fault Tolerant Electrical Power System
 
901804
Automatic Electric Load Management Centers
 
901806
Comparison of DC-10 and MD-11 Designs
 
901955
Development of Applications for the Air Ground Data Exchange Using Mode S Data Link: FAA Program Status
 
901876
Digital Networks And Fiber Optic Interconnection
 
901801
EMI/EMC Considerations with Respect to Distortion Requirements in Aircraft Electric Power Generating Systems
 
901822
Electroluminescent Displays (EL) for General Aviation Cockpits
 
901901
Electromechanical Guidance Fin Actuation in a Four Inch Diameter Air Vehicle
 
901825
Fault-Tolerant Hexad RLG IRU
 
901826
Fiber Optics Based IMU
 
901875
Filter Line Wiring Designs in Aircraft
 
901954
Flight Management Computer System Datalink Interface Capabilities
 
901831
HUD Potential for Narrow-Bodied Air Carrier Aircraft
 
901832
Heads Up Display Applications for Wide Body Transport Aircraft-An Operational Point of View
 
901819
High Performance Modern Avionic Instruments-The LED Flat Panel Display Solution
 
901829
Improving Situational Awareness Through the Use of Intuitive Pictorial Displays
 
901849
Lessons Learned in Control System Integration & Management from the S/MTD Program
 
901796
Redundant, Thin-Wing, High-Pressure, Direct-Drive Valve Actuation System
 
901789
Structural and Thermal Environmental Tests for Electronics: Specification, Purpose, and Selection
 
901833
The HUD as Primary Flight Instrument
 
901787
What is WAT? Wrap Around Test: Maximizing Avionics BIT Utilization to Minimize Flightline Armament System Test Equipment Requirements
 
901048
Advanced Materials Flight Control Actuators
 
901054
Advanced U. S. Military Aircraft Battery Systems
 
901052
High Energy Non-Rechargeable Batteries and their Applications
 
901049
Integrated Control and Avionics for Air Superiority: A Program Overview
 
901055
Nickel Alkaline Batteries for Space Electrical Power Systems
 
901028
Numerical Simulations of Auxiliary Power Units with Different Configurations
 
901056
Sodium-Sulfur Batteries for Satellite Applications
 
901035
Synergy Through Technology Transfer Between Hughes and Delco Electronics
 
901053
Thermal Batteries, Their Technologies and Applications
 
901051
Verification of Flight Critical Systems
 
892357
An Interfacing Solution for Real-Time Avionics Development
 
892219
Analytical Studies for Computed Center Line Operations
 
892226
Considerations for Successful Application of Integrated Drive Generators to Aircraft
 
892227
Design Features of the 747-400 Electric Power System
 
892215
Development of Obstacle Clearance Criteria and Standards for MLS and MLS/RNAV Precision Approaches and Development of an MLS Collision Risk Model
 
892225
EHA Loading on the 270-Vdc Bus
 
892359
Integrated Diagnostics (ID) for Advanced Avionics Architectures
 
892264
Lightweight, Composite Flight Control Actuators
 
892218
MLS RNAV Accuracy Flight Tests
 
892356
Real Time Data Collection and Control in a Distributed Simulator System Using Ethernet TCP/IP
 
892217
Simulation of MLS-ATC Procedures in the New York and San Francisco Terminal Control Areas
 
892216
Simulator Evaluation of “Basic” Mode Back Azimuth Issues in Departure and Missed Approach Usage
 
892326
Software Maintenance on the Airbus Family
 
892327
Use of Onboard Data Loaders
 
892228
VSCF Cycloconverter Reliability Review of the 30/40 KVA F/A-18 Electrical Generating System
 
891052
DESIGN PHILOSOPHY GENERAL AVIATION TCAS DISPLAY
 
891063
Electrochromic Windows: Applications for Aircraft
 
891062
Fatique and Electromagnetic Interference Test for Electro-Impulse De-Icing
 
891086
General Aviation Digital Audio Applications
 
891055
Mode S Transponders - A New Avionics Product
 
891053
Real-Time Decision Making for Autonomous Flight Control
 
891054
Two Effective Methods of Approach and Landing by Visual Display
 
881408
A Highly Reliable DC Power Source for Avionic Subsystems
 
881373
Advanced Flight Control For The Fokker 100
 
881415
Aircraft Automation with an Electronic Library System
 
881374
An Avionics Diagnostics System for Regional Airlines and Business Aircraft Applied in the Beech Starship I
 
881371
Avionics Display Systems
 
881440
Computer-generated Map Display for the Pilot/Vehicle Interface
 
881514
Design and Development of a Software Engineering Training Program
 
881412
Electrical Power System Architectures for Future Aerospace Vehicles
 
881510
Evaluation of Ada Environments
 
881409
Experimental Cascaded Doubly Fed Variable Speed Constant Frequency Generator System
 
881414
High Reliability Aircraft Generator System
 
881411
Overview on the Evolution of Aircraft Battery Systems Used in Air Force Aircraft
 
881410
Parallel Operation of VSCF Electrical Power Generators
 
881417
Sensor Consideration in the Design of a Windshear Detection and Guidance System
 
881513
TestGen-Testing Tool for Ada Designs and Ada Code
 
881407
The All Electric Airplane Revisited
 
881351
The Avionics Integrity Program
 
881370
The Emergence Of Satellite Communication For Commercial Aircraft
 
881413
Unbalanced and Nonlinear Loads in Aircraft Electric Systems
 
881416
Use of Color Displays in the A320 Cockpit
 
872332
A Highly Monitored AV-8B Harrier II Digital Flight Control System
 
872316
Flight Evaluation of an Integrated Control and Display System for High-Precision Manual Landing Flare of Powered-Lift STOL Aircraft
 
872330
Flight Propulsion Control Integration for V/STOL Aircraft
 
872329
Integrated Control and Display Research for Transition and Vertical Flight on the NASA V/STOL Research Aircraft (VSRA)
 
872312
The High Technology Test Bed Program - An Overview
 
872457
Modern Techniques for the Control of RPV's
 
872455
The Study on Eliminating Limit Cycles of a Flight Control System-Adaptive Control and Linear Model Following Approaches
 
871897
A Flight Control System Battle Damage Repair Kit for Control-By-Wire Aircraft
 
871898
Application of Artificial Intelligence Techniques to Sensor Management
 
871812
Candidate FMC/ATC Data Exchange Using Digital Data Communications
 
871887
DC Link VSCF Starter/Generator Systems
 
871810
FMC European Cocktail or Stew?
 
871811
FMCS/TNAV Application in the FAA ATC System
 
871886
Fault-Tolerant Electrical Power System
 
871761
Fly-by-Wire Sidestick Controller Evaluation
 
871884
Modular Packaging of VSCF Converters
 
871885
Power Quality of Aircraft Electric Systems
 
871767
Situation Awareness Metrics Program
 
871768
Vibration Design Criteria for Avionics
 
830714
Fail-Operational DAFCS for Business/Commuter Aircraft
 
810582
The State of the Art of General Aviation Autopilots: Now and in the Future
 
800624
Panel and Back
 
790569
A Demonstration Advanced Avionics System for General Aviation
 
780581
An Electromechanical Actuator Technology Development Program
 
780582
Electromechanical Flight Control Actuation Update
 
770276
Planar Gas Discharge Displays for Automotive Applications
 
750522
Keyboard Data Entry in Avionics
 
750521
Propeller Modulation Effects on a Scanning-Beam Microwave Landing System
 
750206
Temperature Measurement for Advanced Gas Turbine Controls
 
740348
A Unique Approach to the Development of a Light Helicopter Automatic Flight Control System
 
740351
Applications of Fluidics to Light Aircraft Instrumentation and Control
 
740480
Flight/Propulsion Control Integration Aspects of Energy Management
 
740347
Simulation and Flight Evaluation of a Heads-Up Display for General Aviation
 
730331
Development of a Low-Cost Flight Director System for General Aviation
 
730299
Electric Trim Systems: Design and Certification Considerations under FAR 23.677 (CAM 3.337-2)
 
730301
What is Your Altitude?
 
720314
A Solid-State Altitude Encoder
 
720307
TSO Is the Way To Go
 
710380
The Turn Rate Indicator - Its Interpretation as Affected by Installation and True Airspeed
 
700317
American Airlines' Maintenance Recorder Experience
 
700210
CRT Displays for Business Aircraft
 
700213
Flight Control Systems for the Smaller Business Aircraft
 
700584
Interpretation of Test Data by Design Margin Techniques
 
700343
Liquid Metal Servoactuation Packages for Flight Controls
 
700314
Some Historical Highlights of Turbine Engine Condition Monitoring Using Flight Data
 
700344
The Flow Difference Sensor
 
700340
UpSTAGE Missile Flight Control System
 
690407
Design and Development of the Fail Operative Automatic Landing System for the Lockheed L-1011
 
690536
Fluidic Vortex Valve Servoactuators — An Advancement in Helicopter Flight Control Systems
 
690328
Human Factors Evaluation of Aircraft Engine Instrument Displays
 
690406
LAMS B-52 Flight Experiments In Direct Lift Control
 
690326
Outside Looking In Attitude Gyros
 
680207
Open Loop Flight Control System
 
680190
Criteria for Contamination Level in Flight Control Systems
 
670263
A Current Survey of Aircraft Fuel Gauging Systems
 
670255
Automatic Flight Control Development for General Aviation
 
670404
Control Systems for Reusable Launch Vehicles
 
670262
Recent Developments in Instrumentation and Fuel Systems for Turbocharged and/or Pressurized Aircraft
 
670720
The Utility of Human Engineering as Applied to Vehicle Design
 
660191
An Advanced Optical Radar System for Atmospheric Studies
 
660180
Clear Air Turbulence Detection and Warning
 
660175
Clear Air Turbulence: Problems and Solutions (A State-of-the-Art Report)
 
660184
Correlation Between Clear Air Turbulence and Aircraft Electrical Activity
 
660218
Development and Flight Testing a Simplified Fixed Shaft Turboprop Flight Control System
 
660193
Early Warning of Clear Air Turbulence by Photometric Measurements
 
660181
Exploration of the Relationship Between Atmospheric Temperature Change and Clear Air Turbulence
 
660182
Investigation of Techniques for Detecting Clear Air Turbulence
 
660185
Low-Frequency Electrical Characteristics of Clear Air Turbulence
 
660187
Radar Detection of Turbulence in the Upper Troposphere
 
660189
Remote Detection of Clear Air Turbulence by Means of Airborne Infrared Instruments
 
660192
Remote Measurement of Differential Atmospheric Velocity
 
660188
Results Applicable to CAT Detection Using a Millimeter Wave Radiometer Probe
 
660220
The Effect of a Light Aircraft Stability Augmentation System on Pilot Performance
 
660198
The Feasibility of Optical Radar to Detect Clear Air Turbulence
 
650385
The Search for Stability of the Roll Axis
 
640157
Collins 3-D Flight Director System and Peripheral Command Indicator - Status Report
 
640227
LEM FLIGHT CONTROL - A STATEMENT OF THE PROBLEM
 
630369
APPLICATION OF SELF-ADAPTIVE CONTROL TECHNIQUES TO THE FLEXIBLE SUPERSONIC TRANSPORT
 
630571
MINUTEMAN FLIGHT CONTROL SYSTEM THE APPROACH TO AND THE RESULTS OF A FORMAL RELIABILITY PROGRAM
 
620373
Aircraft Instrumentation and Display System-Adaptation of Tactile Link
 
620481
All Mechanical Primary Flight Control System for VTOL/STOL Aircraft
 
620343
Flight Control System Design for Supersonic Transport
 
620444
New Developments in Automatic Landing
 
610368
A Temperature - Response Diagram
 
610005
Applications of Army-Navy Instrumentation Program to Transport Aircraft
 
610245
Gust Simulation As Applied to VTOL Control Problems
 
610370
Integration of Gust Alleviators in Flight Control Systems
 
610369
New Techniques In Automatic Flight Control System Design
 
600346
GENERAL AVIATION DURING THE SOARING SIXTIES
 
600283
PERFORMANCE AND DESIGN CRITERIA OF AN ADAPTIVE CIRCUIT PROPOSED FOR A SPACE RE-ENTRY VEHICLE
 
600250
PILOT INSTRUMENTATION FOR VEHICLE CONTROL IN NEAR SPACE
 
590297
DOPPLER-INERTIAL NAVIGATION FOR HIGH PERFORMANCE AIRCRAFT
 
580136
SOME OF THE NEEDS OF MODERN GENERAL AIRCRAFT AND SOME OF THE POSSIBLE ANSWERS
 
570202
AUTOMATIC FLIGHT CONTROL SYSTEMS REQUIREMENTS FOR HIGH PERFORMANCE FIGHTER AIRCRAFT
 
570218
Cruise Control Instrumentation for Turbojet Aircraft
 
570152
SYSTEMS ANALYSIS APPROACH TO FIREBEE FLIGHT CONTROL SYSTEMS DEVELOPMENT
 
570144
THE ROLE OF DIGITAL COMPUTERS IN AIRBORNE NAVIGATION AND CONTROL
 
560074
AIR MOTOR POWERED HIGH TEMPERATURE ACTUATION SYSTEMS
 
560096
INTEGRATED CONTROL SYSTEMS FOR AIRCRAFT
 
560281
INTEGRATED FLIGHT SYSTEMS
 
560097
THE SYNTHESIS OF AIRCRAFT HYDRAULIC SERVOS
 
550328
ENVIRONMENTAL TESTING OF FUNCTIONAL SYSTEMS
 
540026
A PILOT'S VIEWPOINT OF TURBOJET CONTROL REQUIREMENTS
 
480043
Air Transport Maintenance And Engineering Aspects Of Powerplant Controls
 
480045
Ancestor Worship In Engine Control Design
 
480040
The A- 12 Gyropilot
 
470058
AMERICAN AIRLINES… EVALUATION OF AIRBORNE RADAR
 
470167
Automatons For Tomorrow's Aircraft
 
470131
Standardization And Simplification For The Air Transport Industry
 
460153
THE FUTURE OF AUTOMATIC POWER CONTROLS
 
450165
Basic Principles of POWER BOOST FLIGHT CONTROLS
 
450003
FLIGHT ENGINEER STATION DESIGN AND REQUIREMENTS
 
450026
TRANSOCEANIC AIR NAVIGATION
 
430077
PHILOSOPHY OF FLIGHT TESTING
 
390134
The BMEP Parameter for Airplane Cruising-Power Control
 
380093
ACCESSORIES AND FLYING AIDS CONTRIBUTING TO SAFETY OF OPERATION
 
380019
GROUND TRAINING FOR INSTRUMENT FLYING
 
380028
THE AIR-TRACK SYSTEM OF AIRCRAFT INSTRUMENT LANDING
 
360113
Everyman's Airplane-A Move Toward Simpler Flying
 
340070
AIRCRAFT INSTRUMENTS AND THEIR USES
 
330003
Commercial Flight Tests Improved by New Equipment and Methods
 
320042
Aerial Navigation-Methods and Equipment
 
320043
Flight Control by Air Visualization
 
310036
A Study of Airplane and Instrument- Board Vibration
 
270074
Oversea Navigation
 
170007
AERIAL NAVIGATION OVER WATER
 

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