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SAE International

SAE Papers

Paper Number Paper Title Book Number
2-21-11-20 Aerospace Ergonomics
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 U.S. 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 Demonstration
952042 Fly-By-Light Advanced Systems Hardware (Flash) Program
952028 Mixed Voltage, Microprocessor Based Avionic Systems
952029 Off-The-Shelf Multi-Language Tool Support for Embedded Intel386St 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 Module (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 TodayS Aircraft Into Tomorrow
931593 Modular Electro-Optic Data Bus Coupler
931406 Power Systems 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 Versus 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
912050 Electric Power Generating System for the Boeing 777 Airplane
912107 Els Pilot Evaluation
912111 Els for the A340
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 Elecctromagnetic Interference
912005 Results and Lessons Learned From the Stol and 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 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
901822 Electroluminescent Displays (El) for General Aviation Cockpits
901901 Electromechanical Guidance Fin Actuation in a Four Inch Diameter Air Vehicle
901801 Emi/Emc Considerations With Respect to Distortion Requirments in Aircraft Electric Power Generating Systems
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
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
901831 Hud Potential for Narrow-Bodied Air Carrier Aircarft
901829 Improving Situational Awareness Through the Use of Intuitive Pictorial Displays
901849 Lessons Learned in Control System Integration and 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 Simulation 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
891086 General Aviation Digital Audio Applications
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
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 Solid-State Altitude Encoder
720307 Tso (Technical Standard Order) Is the Way to Go
710380 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
700344 Flow Difference Sensor Can Protect Hydraulic Systems of Battle Damaged Aircraft
700584 Interpretation of Test Data By Design Margin Technique
700343 Liquid Metal Servoactuation Packages for Flight Controls
700314 Some Historical Highlights of Turbine Engine Condition Monitoring Using Flight Data
700340 Upstage Missile Flight Control System
690406 B-52 Flight Experiments in Direct Lift Control Under the Load Alleviation and Mode Stabilization Advanced Development Program
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
690326 Outside Looking in Attitude Gyros
680207 Open loop automatic flight control system
680190 Criteria for Contamination Level in Flight Control Systems
670255 Automatic Flight Control Developments for General Aviation
670404 Control Systems for Reusable Launch Vehicles
670720 Utility of Human Engineering as Applied to Vehicle Design
660180 Advance Detection and Warning of Clear Air Turbulence By Airborne Devices
660191 Advanced Optical Radar System for Atmospheric Studies
660188 Clear Air Turbulence Detection Using a Millimeter Wave Radiometer Probe
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
660220 Effect of a Light Aircraft Stability Augmentation System on Pilot Performance
660181 Exploration of the Relationship Between Atmospheric Temperature Change and Clear Air Turbulence
660198 Feasibility of Pulsed Ruby Laser Optical Radar to Detect 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
660175 Report of Clear Air Turbulence Problems and Solutions
670263 Current Survey of Aircraft Fuel Gaging Systems
670262 Recent Developments in Instrumentation and Fuel Systems for Turbocharged And/Or Pressurized Aircraft
650385 Search for Roll Axis Stability
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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