Equipment and operational concepts affecting aircraft in the terminal area are reported. Curved approach applications and modified climb and descent procedures for minimum fuel consumption are considered. The curved approach study involves the application of MLS guidance to enable execution of the current visual approach to Washington National Airport under instrument flight conditions. The operational significance and the flight path control requirements involved in the application of curved approach paths to this situation are considered. Alternative flight path control regimes are considered to achieve minimum fuel consumption subject to constraints related to air traffic control requirements, flight crew and passenger reactions, and air...
Analyses of McDonnell Douglas DC-8, DC-9, and DC-10 jet transports were conducted to investigate the...
A flight control system concept is defined for approach flightpath control of an augmentor wing (or ...
Computer capability weather input data, performance data, and ATC interface are discussed in terms o...
Rising fuel costs combined with other economic pressures have resulted in industry requirements for ...
A flight investigation using a De Havilland Twin Otter airplane was conducted to determine the confi...
Operational procedures for use in an assumed short haul transport route were evaluated. The curved p...
Flight test of steep instrument approach performance of manually controlled C- 47 aircraf
A real-time, fixed-base simulation study has been conducted to determine the curved, descending appr...
A system which is capable of controlling an aircraft automatically along a curved, descending, decel...
Hardware and software requirements for an Approach Energy Management System (AEMS) consisting of an ...
The terminal guidance system (TGS) is avionic equipment which gives guidance along a curved descendi...
The NASA Terminal Configured Vehicle is a flying laboratory used to conduct research and development...
The control, display, and procedural features are described for a flight experiment conducted to ass...
The XV-5B lift-fan aircraft was used to explore the factors affecting handling qualities in the term...
The results of an engineering and piloted simulator study to adapt a NASA developed-approach energy ...
Analyses of McDonnell Douglas DC-8, DC-9, and DC-10 jet transports were conducted to investigate the...
A flight control system concept is defined for approach flightpath control of an augmentor wing (or ...
Computer capability weather input data, performance data, and ATC interface are discussed in terms o...
Rising fuel costs combined with other economic pressures have resulted in industry requirements for ...
A flight investigation using a De Havilland Twin Otter airplane was conducted to determine the confi...
Operational procedures for use in an assumed short haul transport route were evaluated. The curved p...
Flight test of steep instrument approach performance of manually controlled C- 47 aircraf
A real-time, fixed-base simulation study has been conducted to determine the curved, descending appr...
A system which is capable of controlling an aircraft automatically along a curved, descending, decel...
Hardware and software requirements for an Approach Energy Management System (AEMS) consisting of an ...
The terminal guidance system (TGS) is avionic equipment which gives guidance along a curved descendi...
The NASA Terminal Configured Vehicle is a flying laboratory used to conduct research and development...
The control, display, and procedural features are described for a flight experiment conducted to ass...
The XV-5B lift-fan aircraft was used to explore the factors affecting handling qualities in the term...
The results of an engineering and piloted simulator study to adapt a NASA developed-approach energy ...
Analyses of McDonnell Douglas DC-8, DC-9, and DC-10 jet transports were conducted to investigate the...
A flight control system concept is defined for approach flightpath control of an augmentor wing (or ...
Computer capability weather input data, performance data, and ATC interface are discussed in terms o...