Metering and spacing (M & S) system's algorithms described assume an aircraft two dimensional are navigation capability. The three navigation systems compared were: very high frequency omnidirectional range/distance measuring equipment (VOR/DME) and ILS, VOR/DME and + or - 40 MLS, and VOR/DME and + or - 60 MLS. Other factors studied were M & S tentative schedule point location, route geometry effects, and approach gate location effects. Summarized results are: the MLS offers some improvement over VOR/DME and ILS if all approach routes contain computer assisted turns; pilot reaction to moving the gate closer to the runway threshold may adversely affect M & S performance; and coupling en route metering to terminal scheduling transfers most of...
A 75 flight-hour operational evaluation was conducted with a representative four-engine fan-jet tran...
Computer simulation results are presented for intercepting final approach paths using various Microw...
Alternative types of communication systems for deep space probes and extent of aid spacecraft can pr...
The results of an investigation made to assess the Microwave Landing System (MLS) Requirements for u...
Analysis, modeling, and simulations were conducted as part of a multiyear investigation of the more ...
The objective of this study was to identify crew procedures involved in Microwave Landing System (ML...
The characteristics and performance of MLS equipment utilized by the TCV B-737. Several classes of M...
Results for the Microwave Landing System (MLS) guidance algorithm development conducted under the Ad...
The TAEM guidance and body rotational dynamics models required for the MCC simulation of the TAEM mi...
The problems in navigation and guidance encountered by aircraft in the initial transition period in ...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...
Transmission loss from precipitation scatter interference between space and earth communication syst...
The necessary algorithms to reconstruct the glideslope change waypoint along a straight line in the ...
Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle ...
Simulation and flight tests were conducted to compare the accuracy of two algorithms designed to com...
A 75 flight-hour operational evaluation was conducted with a representative four-engine fan-jet tran...
Computer simulation results are presented for intercepting final approach paths using various Microw...
Alternative types of communication systems for deep space probes and extent of aid spacecraft can pr...
The results of an investigation made to assess the Microwave Landing System (MLS) Requirements for u...
Analysis, modeling, and simulations were conducted as part of a multiyear investigation of the more ...
The objective of this study was to identify crew procedures involved in Microwave Landing System (ML...
The characteristics and performance of MLS equipment utilized by the TCV B-737. Several classes of M...
Results for the Microwave Landing System (MLS) guidance algorithm development conducted under the Ad...
The TAEM guidance and body rotational dynamics models required for the MCC simulation of the TAEM mi...
The problems in navigation and guidance encountered by aircraft in the initial transition period in ...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...
Transmission loss from precipitation scatter interference between space and earth communication syst...
The necessary algorithms to reconstruct the glideslope change waypoint along a straight line in the ...
Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle ...
Simulation and flight tests were conducted to compare the accuracy of two algorithms designed to com...
A 75 flight-hour operational evaluation was conducted with a representative four-engine fan-jet tran...
Computer simulation results are presented for intercepting final approach paths using various Microw...
Alternative types of communication systems for deep space probes and extent of aid spacecraft can pr...