All Stories

  1. Aero-Propulsion Control Research in Support of NASA Aeronautics Strategic Research Thrusts
  2. Aircraft Engine Advanced Controls Research under NASA Aeronautics Research Mission Programs
  3. Aero-propulsion Controls Research
  4. Aircraft Turbine Engine Control Research at NASA Glenn Research Center
  5. Reducing Conservatism in Aircraft Engine Response Using Conditionally Active Min-Max Limit Regulators
  6. Intelligent Propulsion Control and Health Management
  7. Application of an Optimal Tuner Selection Approach for On-Board Self-Tuning Engine Models
  8. Propulsion Controls and Diagnostics Research in Support of NASA Aeronautics Research Mission Programs
  9. Sensor and Actuator Needs for More Intelligent Gas Turbine Engines
  10. A Systematic Approach for Model-Based Aircraft Engine Performance Estimation
  11. Optimal Tuner Selection for Kalman Filter-Based Aircraft Engine Performance Estimation
  12. Propulsion Health Management System Development for Affordable and Reliable Operation of Space Exploration Systems
  13. Implementation Challenges for Multivariable Control: What you did not learn in school!
  14. Propulsion Controls and Diagnostics Research at NASA Glenn
  15. Controls and Health Management Technologies for Intelligent Aerospace Propulsion Systems
  16. Sensor Needs for Control and Health Management of Intelligent Aircraft Engines
  17. An optimized integrator windup protection technique applied to a turbofan engine control
  18. Turbofan engine control design using robust multivariable control technologies
  19. A Comparison of Multivariable Control Design Techniques for a Turbofan Engine Control
  20. Application of controller partitioning optimization procedure to integrated flight/propulsion control design for a STOVL aircraft
  21. Robust integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques
  22. Propulsion system performance resulting from an Integrated Flight/Propulsion Control design
  23. Neural network application to aircraft control system design
  24. H-infinity based integrated flight/propulsion control design for a STOVL aircraft in transition flight
  25. Experimental investigation of control/display augmentation effects in a compensatory tracking task
  26. Cooperative synthesis of control and display augmentation for a STOLaircraft in the approach and landing task
  27. Comments on ‘The phenomenon of homeopathic instability in dynamical systems’