Landings by experienced airline pilots transitioning to the DC-10, performed in flight and on a simulator, were analyzed and compared using a pilot-in-the-loop model of the landing maneuver. By solving for the effective feedback gains and pilot compensation which described landing technique, it was possible to discern fundamental differences in pilot behavior between the actual aircraft and the simulator. These differences were then used to infer simulator fidelity in terms of specific deficiencies and to quantify the effectiveness of training on the simulator as compared to training in flight. While training on the simulator, pilots exhibited larger effective lag in commanding the flare. The inability to compensate adequately for this lag ...
An automatic landing system was developed for the Augmentor Wing Jet STOL Research Airplane to estab...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
A piloted flight simulator experiment was conducted to evaluate issues related to the display of mic...
As part of an ongoing government and industry effort to study the flying qualities of aircraft with ...
This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehic...
A flightworthy active control landing gear system for a supersonic aircraft was designed to minimize...
Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity re...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
A technique was developed which provides reliable failure detection and identification (FDI) for a d...
Fast Fourier Transform (FFT) and Least Square Error (LSE) estimation techniques were applied to the ...
The advantages and disadvantages of head-up displays (HUDs) in commercial jet transport approach and...
Partial failures of aircraft primary flight control systems and structural damages to aircraft durin...
A modular computer program (ANOPP) for predicting aircraft flyover and sideline noise was developed....
abstract: This thesis explores the human factors effects pilots have when controlling the aircraft d...
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
An automatic landing system was developed for the Augmentor Wing Jet STOL Research Airplane to estab...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
A piloted flight simulator experiment was conducted to evaluate issues related to the display of mic...
As part of an ongoing government and industry effort to study the flying qualities of aircraft with ...
This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehic...
A flightworthy active control landing gear system for a supersonic aircraft was designed to minimize...
Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity re...
The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the B...
A technique was developed which provides reliable failure detection and identification (FDI) for a d...
Fast Fourier Transform (FFT) and Least Square Error (LSE) estimation techniques were applied to the ...
The advantages and disadvantages of head-up displays (HUDs) in commercial jet transport approach and...
Partial failures of aircraft primary flight control systems and structural damages to aircraft durin...
A modular computer program (ANOPP) for predicting aircraft flyover and sideline noise was developed....
abstract: This thesis explores the human factors effects pilots have when controlling the aircraft d...
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
An automatic landing system was developed for the Augmentor Wing Jet STOL Research Airplane to estab...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
A piloted flight simulator experiment was conducted to evaluate issues related to the display of mic...