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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
2008-01-2256
A Brief Study of Conditionally Enabled Phase Compensated Rate Limiters
 
2008-01-2253
Aircraft Performance Prediction: Comparison of Classical Handbook Methods to Detailed Time Integration Computer-Aided Methods
 
2008-01-2254
Cost Benefits of Aerodynamic Data Generation Techniques for Aircraft Stability and Control Analysis using the J2 Universal Tool-Kit
 
2008-01-2271
Dynamic Taxonomies Usage in the Context of Aeronautical Maintenance Processes to Increase the Effectiveness and the Efficiency of the Operations
 
2008-01-2272
Finite Element Modeling Strategies for Dynamic Aircraft Seats
 
2008-01-2265
Having 5000 Destinations in the Modern U.S. Airways System
 
2008-01-2263
Jam-Free, Fail-Safe Flight Control System with Asymmetric Load Alleviation Capability
 
2008-01-2262
Keys to Success with Knowledge-based Techniques
 
2008-01-2230
Model-Driven Architecture for Platform and Store Design
 
2008-01-2270
Modern Solutions for Ground Vibration Testing of Small, Medium and Large Aircraft
 
2008-01-2260
Reduction of Jitter within Optical Tracking Data through an In-depth Survey of Smoothing Techniques
 
2008-01-2261
Testing a Nonveridical Aircraft Collision Avoidance System
 
2008-01-2264
The Seven Parameters of Highly Effective Cable Control Systems
 
2008-01-2255
Three-Movement Handlebar Piloting Control
 
2001-01-2965
Advanced Real-time Aerodynamic Model Identification Technique
 
2001-01-2988
Analytical and Numerical Modelling of the Turn Maneuver of Agricultural Aircraft
 
2000-01-3226
Design of an Active Feel System for a Flight Simulator
 
2000-01-5501
Certification Flight Test for an Extended Range Modification for the Cessna 337 Aircraft
 
2000-01-5500
MICCO Mac-145B Spin Flight Test
 
2000-01-5619
Modifications Required to Convert a U.S. Registered Aircraft for European Operations
 
2000-01-5523
Propulsion Flight Testing on General Electric's B747 Flying Test Bed
 
2000-01-5502
The Bombardier Flight Test Center - Meeting the Challenge
 
985556
High Stability Engine Control (HISTEC): Flight Demonstration Results
 
985592
Recent NASA Wake-Vortex Flight Tests, Flow-Physics Database and Wake-Development Analysis
 
981817
Analysis of Salient Events from the Two-Phase Flow (TPF) Thermal Control Flight Experiment
 
981548
Thermal Control of a Large Deployable Antenna on the HALCA Satellite
 
981209
A Simple Takeoff Monitor
 
975523
Maturing Fighter Engines Through Flight Testing
 
975603
Aircar Driving and Model Flight Test Update
 
892355
Managing Man-in-the-Loop Simulations
 
892284
Simulation Evaluation of Transition and Hover Flying Qualities of a Mixed-Flow, Remote-Lift STOVL Aircraft
 
881485
A VSAERO Analysis of Several Canard Configured Aircraft
 
881433
The Current Status of the Flight Test of the ASKA
 
871895
8000 psi Hydraulic System Seals and Materials Test Program-Final Report
 
871875
Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft
 
871800
In-Flight Environmental Effects on Airplane Composite Vertical Fin Caps
 
871863
Microprocessor Control of Aerospace Hydraulic Pumps
 
871908
Shuttle and ELV Flight Planning Using the Flight Design System
 
871749
The Effect of Helicopter Vibration on the Accuracy of a Voice Recognition System
 
861685
Supersonic Cruise Technology Roadmap
 
861650
A Cooperative Launch Optimization Technique Using the Flight Design System
 
861671
Evaluation of Composite Components on the Bell 206L and Sikorsky S-76 Helicopter
 
861816
Flight Simulators in Aerospace Engineering Education
 
861803
Flight Testing TECS — The Total Energy Control System
 
861823
Testing and Instrumentation Used in the AN/APG-67 Multimode Radar
 
851771
The X-29 - a Unique and Innovative Aerodynamic Concept
 
851956
Cockpit Automation: In Need of a Philosophy
 
851991
Interactive Computer-Based Flight Training
 
851964
Ada for Simulators
 
851903
Application of the Optimal Control Model to the Design of Flight Simulation Experiments
 
851944
Capabilities of Airborne and Ground Based Flight Simulation
 
851824
DIGITAC II - Architecture and Redundancy Management
 
851826
DIGITAC Multimode Control Laws
 
851865
Flight Planning with the NASA Flight Design System
 
851910
Lightweight Hydraulic System Technology-8000 PSI Update
 
851965
Simulation of Aircraft Components for Training Purposes
 
851827
USAF Test Pilot School Use of DIGITAC in Systems Testing
 
851946
Visual Cue Dominance Hierarchies: Implications for Simulator Design
 
841492
A Review of Pilot Workload Measurement Techniques Used on the A-10 Single Seat Night Attack Test Program
 
841533
AI Applications to Military Pilot Decision Aiding—A Perspective on Transition
 
841633
Advanced Fighter Technology Integration (AFTI) F-16–The Pilot Interface
 
841534
Automation in the Cockpit: Who's in Charge?
 
841611
Comparison of Voice Types for Helicopter Voice Warning Systems
 
841610
Development of an Advanced Helicopter Research Simulator
 
841489
Effects of Digital Altimetry on Pilot Workload
 
841467
Electronic Display of Powerplant Parameters
 
841471
Flight Deck Automation Decisions
 
841472
Flight Deck Design Methodology Using Computerized Anthropometric Models
 
841490
Problems in New Cockpit Certification
 
841553
Propulsion Control Experience Used in the Highly Integrated Digital Electronic Control (HIDEC) Program
 
841597
Simulator Sickness: A Survey of Flight Simulators for the Navy
 
841620
Space Shuttle Mission Extension Capability
 
841450
Tactical Flight Management—An Overview
 
841632
YA-10B Single Seat Night Attack: Lessons Learned
 
831411
Digital Flight Control System EMI/EMP Testing-Lessons Learned
 
831472
F-15 Dual Role Fighter Cockpit Integration
 
831459
Improving the Operator Interface Through Use of a Touch Interactive Display
 
831469
Predictive Controller Issues for Trajectory Control
 
831533
Primary Flight Display: A Step Beyond EADI's
 
831425
STOL and Maneuver Technology Program
 
831466
The Scientific Approach and Cockpit Design - They are Compatible
 
831445
The Use of Holographic Head-Up Display of Flight Path Symbology in Varying Weather Conditions
 
831457
Voice Interactive Systems Technology Assessment
 
821385
Advanced Technology in the Flight Station
 
821447
FAA's Trend Analysis Data System
 
821341
NGT Sub-Scale Flight Demonstrator — A Cost-Effective Approach to Aircraft Development
 
821354
Space Transportation System Payload Flight Data File
 
821448
The Aviation Safety Analysis System (ASAS): An Overview
 
821450
The Impact of Automation on Flight Test
 
821352
The Pilot's Role in Manned Space Flight
 
801182
Application of Performance Based Feedback to Air Combat Training
 
801219
Current and Future Use of an AIDS Integrated EMS
 
801205
Evaluation of Several Control/Display Concepts for V/STOL Shipboard Landing
 
801184
Trends In Air Force Simulation — Perspective from the Air Force Human Resources Laboratory Operations Training Division
 
801206
Velocity Command/Position Hold: A New Flight Control Concept for Hovering VTOL Aircraft
 
791083
Control System Techniques for Improved Departure/Spin Resistance for Fighter Aircraft
 
781004
Naval Aviation Training - Perspective and Prospects
 
781007
Recent Developments and Plans for Pilot Training Devices
 
770995
Concorde AIDS - Powerplant Applications
 
760884
An Approach to a Methodology for Selection and Development of Flight/Propulsion Control Coupling Technologies
 
760933
Procedures Used In Flight Tests of an Integrated Propulsion Control System on an F-111E Airplane
 
760931
Simulation's Potential Role in Advanced Aircraft Certification
 
760934
T700 Engine Flight Test Experience on UTTAS and AAH
 
760887
The HiMAT RPRV Propulsion Control System
 
760932
YJ101/YF-17 Flight Test Experience
 
740873
Missile Guidance and Control System Design Trends
 
740824
Supersonic Inlet Simulator - A Tool for Simulation of Realistic Engine Entry Flow Conditions
 
730947
Evaluation of V/STOL Research Aircraft Design
 
730987
Flight Control System Advances for Near-Future Military Aircraft
 
730988
Fluid Power and Control Requirements for the U. S. Army Heavy Lift Helicopter
 
730933
Use of Simulators in the Design and Development of Flight Control Systems
 
720854
Combat Capabilities and Versatility Through CCV
 
720858
Flight Simulator Development in Parallel with Aircraft Flight Test - A Case Study of the American Airlines DC-10 Program
 
700830
DC-10 Test Program Effectiveness
 
700794
Development of a Hybrid Fluidic Damper Control for an Aircraft Yaw Axis
 
700793
Hydrofluidic Flight Controls
 
690678
Integrated Flight Test Data System With Real-Time Graphic Display
 
690614
An Integrated Aerospace Dynamic Program
 
690675
Development Testing of the New Generation of Large Jet Aircraft
 
690670
Hydraulic System State-of-the-Art Advances on the 747 Airplane
 
690690
VERSATILE LAUNCH VEHICLE DIGITAL AUTOPILOT
 
670311
A Review of the Current Policy in the United Kingdom for the Use of Flight Simulators in Flight Crew Training and Checking
 
670305
Aerospace Concepts Applied to Deep Submergence Vehicle Simulation
 
670304
Flight Simulator Motion, Its Enhancement and Potential for Flight Crew Training
 
670301
Future Potential and Requirements of Digital Simulation
 
670307
SST Training Program Considerations
 
670300
Survey of Flight Simulation Computation Methods
 
670269
Test Results of an All-Mechanical Flight Control System Utilizing a Cascade Toroidal Servo
 
670297
The Urgent Need for Flight Simulators for Present and Future Aircraft
 
670303
Visual Simulation - Where We Are - Where We Are Going
 
670571
XC-142A Control System
 
660315
A Report on Stability and Control Testing of a Tilt Wing V/STOL Aircraft
 
650231
1953 Paper Jet Operations in Retrospect with Connotations for the Supersonic Transport
 
650570
A Fail-Operative Stability Augmentation System with Self-Test Capability
 
650350
A Hot Gas Servocontrol System for Aerospace Applications
 
650338
A Stored Gas Actuator Unit for the TOW Missile
 
650580
Analysis of Toroidal Actuation Systems for Aerospace Vehicles
 
650600
Applied Fluids Technology
 
650572
Automatic Landing Systems Mechanization - Series or Parallel Servos?
 
650808
Control Requirements and Control Methods for Large V/STOL Aircraft
 
650573
Development of Failure-Correcting Flight Control System
 
650582
Difficulties in Control System Synthesis for Launch Vehicles Exhibiting Severe Mode Interaction
 
650205
Flight Simulator Utilization for System Design and Pilot Training
 
650848
Flight Testing the 707 Automatic Landing System
 
650598
Functional Design of the Minuteman Flight Control System
 
650595
Gemini Flight Control System Performance during the Second Unmanned Flight
 
650575
HydroLogic Redundant Systems
 
650811
Manned Control - Direct and Remote
 
650830
Reaction Control Systems for V/STOL Aircraft
 
650798
Technological Advancements Resulting from XB-70 Performance Requirements
 
650579
The Balanced-Power Actuation Concept
 
650574
The Potential of Monitorless Control Systems of High Redundancy Efficiency
 

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