Several guidance and control system research and development activities aimed at improving the operational capabilities of commercial aircraft in the terminal area are described. The guidance and control systems were designed to improve the capacity and efficiency of terminal area operations, enhance the approach and landing capability of aircraft in adverse weather conditions, and reduce the impact of aircraft noise perceived on the ground. Specific performance features include the ability to capture and track steep glideslopes, use short final approaches, perform flares with reduced longitudinal touchdown dispersion and execute high speed runway rollout and turnoff. Results obtained from simulation studies or flight tests are shown for ea...
The effect on pilot scan behavior of both advanced cockpit and advanced manuevers was assessed. A se...
Stochastic control theory is applied to the problem of designing a digital flight compensator for te...
Steep instrument approach capabilities of T-33 airplane under manual control from glide slope to tou...
The NASA Terminal Configured Vehicle is a flying laboratory used to conduct research and development...
A digital avionics system was installed in the CV-340 transport aircraft. Flight tests were made to ...
The terminal guidance system (TGS) is avionic equipment which gives guidance along a curved descendi...
Terminal-area guidance problems are solved in the form of computer-oriented algorithms. A flyable, t...
A concept for automating the control of air traffic in the terminal area in which the primary man-ma...
A piloted simulator was used to evaluate the flight path angle control capabilities of a system that...
Evaluation of automatic guidance modes and software for V/STOL aircraft flight contro
To determine the advantages and disadvantages of head-up displays (HUD) in civil transport approach ...
The characteristics of air traffic patterns at uncontrolled airports and techniques used by a group ...
The objective was to design a control logic which automates all or part of the guidance function for...
A study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader...
A computerized analysis procedure, based on a control theoretic model of the human pilot, is used to...
The effect on pilot scan behavior of both advanced cockpit and advanced manuevers was assessed. A se...
Stochastic control theory is applied to the problem of designing a digital flight compensator for te...
Steep instrument approach capabilities of T-33 airplane under manual control from glide slope to tou...
The NASA Terminal Configured Vehicle is a flying laboratory used to conduct research and development...
A digital avionics system was installed in the CV-340 transport aircraft. Flight tests were made to ...
The terminal guidance system (TGS) is avionic equipment which gives guidance along a curved descendi...
Terminal-area guidance problems are solved in the form of computer-oriented algorithms. A flyable, t...
A concept for automating the control of air traffic in the terminal area in which the primary man-ma...
A piloted simulator was used to evaluate the flight path angle control capabilities of a system that...
Evaluation of automatic guidance modes and software for V/STOL aircraft flight contro
To determine the advantages and disadvantages of head-up displays (HUD) in civil transport approach ...
The characteristics of air traffic patterns at uncontrolled airports and techniques used by a group ...
The objective was to design a control logic which automates all or part of the guidance function for...
A study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader...
A computerized analysis procedure, based on a control theoretic model of the human pilot, is used to...
The effect on pilot scan behavior of both advanced cockpit and advanced manuevers was assessed. A se...
Stochastic control theory is applied to the problem of designing a digital flight compensator for te...
Steep instrument approach capabilities of T-33 airplane under manual control from glide slope to tou...