In contrast to CTOL landing operations, STOL airplanes landing on short STOLport runways typically begin the flare maneuver before reaching the runway surface. Vertical guidance procedures were developed to allow an autoland flight control system for a STOL airplane to use Microwave Landing System (MLS) signals as altitude and sink rate references for flare initiation, with a transition to radar altimeter after the airplane is over the runway. The implementation has minimum impact on the control system and landing performance. Data are presented which show validation of the concepts in a simulator
Configurations of MLS Flare Elevation Systems that can be considered reasonable and practical in act...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...
A real-time, fixed-base simulation study has been conducted to determine the curved, descending appr...
A series of investigations were conducted to generate and verify through ground bases simulation and...
Simulated instrument approaches were made to Category 1 minimums followed by a visual landing on a 1...
Advanced automatic flare and decrab control laws were developed for future powered lift STOL aircraf...
Automatic flare and decrab control laws were developed for NASA's experimental Twin Otter. This ligh...
A digital avionics system referred to as STOLAND has been test-flown in the NASA CV-340 to obtain pe...
A flight investigation using a De Havilland Twin Otter airplane was conducted to determine the confi...
Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertic...
The results of an investigation made to assess the Microwave Landing System (MLS) Requirements for u...
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
A longitudinal digital guidance and control law for steep glideslopes using MLS (Microwave Landing S...
An automatic go-around control system was evaluated on the Augmentor Wing Jet Short Takeoff and Land...
Configurations of MLS Flare Elevation Systems that can be considered reasonable and practical in act...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...
A real-time, fixed-base simulation study has been conducted to determine the curved, descending appr...
A series of investigations were conducted to generate and verify through ground bases simulation and...
Simulated instrument approaches were made to Category 1 minimums followed by a visual landing on a 1...
Advanced automatic flare and decrab control laws were developed for future powered lift STOL aircraf...
Automatic flare and decrab control laws were developed for NASA's experimental Twin Otter. This ligh...
A digital avionics system referred to as STOLAND has been test-flown in the NASA CV-340 to obtain pe...
A flight investigation using a De Havilland Twin Otter airplane was conducted to determine the confi...
Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertic...
The results of an investigation made to assess the Microwave Landing System (MLS) Requirements for u...
Simulation tests were made using an experimental powered-lift STOL airplane to help define airport-a...
A longitudinal digital guidance and control law for steep glideslopes using MLS (Microwave Landing S...
An automatic go-around control system was evaluated on the Augmentor Wing Jet Short Takeoff and Land...
Configurations of MLS Flare Elevation Systems that can be considered reasonable and practical in act...
A fixed-base simulator study was conducted to determine the minimum acceptable level of longitudinal...
Results of simulated precision departures and missed approaches using MLS guidance concepts are pres...