Add to ORKGA description of the simulation program used to study the landing approach, rollout and turnoff of the B737-100 aircraft utilizing MLS and a buried magnetic leader cable as navigation aids is presented. Simulation results are given and show the concept to be both feasible and practical for commercial type aircraft terminal area control
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Tra...
This report defines the initial requirements for designing a research high-speed rollout and turnoff...
An experimental magnetic leader cable (MLC) system designed to measure aircraft lateral displacement...
A study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader...
The problems in navigation and guidance encountered by aircraft in the initial transition period in ...
Issued Oct. 1977.Prepared by Analytical Mechanics Associates for Langley Research Center under contr...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...
The necessary algorithms to reconstruct the glideslope change waypoint along a straight line in the ...
Tests were conducted with a van mounted experimental magnetic leader cable sensor to evaluate its po...
The development of a digital automatic control law for a small jet transport to perform a steep fina...
The research to develop and fabricate a terminal area navigation system for use in the NASA VTOL App...
In contrast to CTOL landing operations, STOL airplanes landing on short STOLport runways typically b...
Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertic...
The design, development, implementation and flight tests of the Digital Integrated Automatic Landing...
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Tra...
This report defines the initial requirements for designing a research high-speed rollout and turnoff...
An experimental magnetic leader cable (MLC) system designed to measure aircraft lateral displacement...
A study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader...
The problems in navigation and guidance encountered by aircraft in the initial transition period in ...
Issued Oct. 1977.Prepared by Analytical Mechanics Associates for Langley Research Center under contr...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...
The necessary algorithms to reconstruct the glideslope change waypoint along a straight line in the ...
Tests were conducted with a van mounted experimental magnetic leader cable sensor to evaluate its po...
The development of a digital automatic control law for a small jet transport to perform a steep fina...
The research to develop and fabricate a terminal area navigation system for use in the NASA VTOL App...
In contrast to CTOL landing operations, STOL airplanes landing on short STOLport runways typically b...
Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertic...
The design, development, implementation and flight tests of the Digital Integrated Automatic Landing...
Minimizing performance criterion to analyze ability of automatically controlled aircraft to maintain...
Five flight tests of the Digital Automated Landing System (DIALS) were conducted on the Advanced Tra...
This report defines the initial requirements for designing a research high-speed rollout and turnoff...