Westinghouse conducted a flight test with its Sabreliner AN/APG-68 instrumented radar to assess the urban discrete/ground moving vehicle clutter environment. Glideslope approaches were flown into Washington National, BWI, and Georgetown, Delaware, airports employing radar mode timing, waveform, and processing configurations plausible for microburst windshear avoidance. The perceptions, both general and specific, of the clutter environment furnish an empirical foundation for beginning low false alarm detection algorithm development
For substantiation of the recently certified medium range Airbus A330 and long range A340 the full s...
A summary of findings of the Flight Elements Subpanel is given in viewgraph form. Topics covered inc...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
Using a two-dimensional linear least-squares method applied to Doppler radar data, we test the viabi...
Delco Systems' Forward Looking Windshear Detection program is reviewed in viewgraph form. Topics cov...
Previous studies have shown graphical presentation methods of hazardous wind shear to be superior to...
Ground clutter interference is a major problem for airborne pulse Doppler radar operating at low alt...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
A portable microcomputer data system was developed to test a 2 x 64-element Si:Bi charge injection d...
The Terminal Doppler Weather Radar (TDWR) testbed system was operated during the months of July to A...
Wind shear detection status is presented in the form of view-graphs. The following subject areas are...
This pictorial presentation reviews the post-flight analysis results from two type of hardware (tray...
A task order was written by the High Resolution, High Frame Rate Video Technology (HHVT) project eng...
The objective is to advance the state of the art in onboard image data processing and storage throug...
A wake vortex avoidance system includes a microphone array configured to detect low frequency sounds...
For substantiation of the recently certified medium range Airbus A330 and long range A340 the full s...
A summary of findings of the Flight Elements Subpanel is given in viewgraph form. Topics covered inc...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...
Using a two-dimensional linear least-squares method applied to Doppler radar data, we test the viabi...
Delco Systems' Forward Looking Windshear Detection program is reviewed in viewgraph form. Topics cov...
Previous studies have shown graphical presentation methods of hazardous wind shear to be superior to...
Ground clutter interference is a major problem for airborne pulse Doppler radar operating at low alt...
As a result of high cycle fatigue, hydrogen embrittlement, and extended engine use, it was observed ...
A portable microcomputer data system was developed to test a 2 x 64-element Si:Bi charge injection d...
The Terminal Doppler Weather Radar (TDWR) testbed system was operated during the months of July to A...
Wind shear detection status is presented in the form of view-graphs. The following subject areas are...
This pictorial presentation reviews the post-flight analysis results from two type of hardware (tray...
A task order was written by the High Resolution, High Frame Rate Video Technology (HHVT) project eng...
The objective is to advance the state of the art in onboard image data processing and storage throug...
A wake vortex avoidance system includes a microphone array configured to detect low frequency sounds...
For substantiation of the recently certified medium range Airbus A330 and long range A340 the full s...
A summary of findings of the Flight Elements Subpanel is given in viewgraph form. Topics covered inc...
An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fusel...