This paper describes recent results from a partnership between the Sikorsky Aircraft Corporation and the Georgia Institute of Technology to develop, improve, and flight test a sensor, guidance, navigation, control, and real-time flight path optimization system to support high performance nap-of-the-Earth helicopter flight. The emphasis here is on optimization for a combination of low height above terrain/obstacles and high speeds. Multiple methods for generating the desired flight path were evaluated, including (1) a simple processing of each laser scan; and (2) a potential field based method. Simulation and flight test results have been obtained utilizing an onboard laser scanner to detect terrain and obstacles while flying at low al...
Abstract — Safe autonomous flight is essential for widespread acceptance of aircraft that must fly c...
NASA and the U.S. Army are jointly developing a teleoperated unmanned rotorcraft research platform a...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...
Through combining environmental sensing by the use of LIDAR, RADAR, stereo vision and other similar ...
Rotorcraft operating in high-threat environments fly close to the earth's surface to utilize surroun...
NASA and the U.S. Army have designed, developed, and flight evaluated a Computer Aiding for Low Alti...
The Flight Systems Development branch of the U.S. Army's Avionics Research and Development Activity ...
A computer aiding concept for low-altitude helicopter flight was developed and evaluated in a real-t...
https://doi.org/10.21949/14033301994PDFTech ReportHelicopter pilotsInformation display systemsHead u...
A computer-aiding concept for low-altitude helicopter flight was developed and evaluated in a real-t...
Automated low-altitude flight and landing in remote areas within a civilian environment are investig...
In the last years UAV (Unmanned Aerial Vehicle) systems are become very actractive for various comme...
Work being accomplished to develop a real-time, piloted simulation of a helicopter using the vertica...
The ability to fly at low altitude while actively avoiding collisions with the terrain and objects s...
Helicopter flight is among the most demanding of all human-machine integrations. The inherent manual...
Abstract — Safe autonomous flight is essential for widespread acceptance of aircraft that must fly c...
NASA and the U.S. Army are jointly developing a teleoperated unmanned rotorcraft research platform a...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...
Through combining environmental sensing by the use of LIDAR, RADAR, stereo vision and other similar ...
Rotorcraft operating in high-threat environments fly close to the earth's surface to utilize surroun...
NASA and the U.S. Army have designed, developed, and flight evaluated a Computer Aiding for Low Alti...
The Flight Systems Development branch of the U.S. Army's Avionics Research and Development Activity ...
A computer aiding concept for low-altitude helicopter flight was developed and evaluated in a real-t...
https://doi.org/10.21949/14033301994PDFTech ReportHelicopter pilotsInformation display systemsHead u...
A computer-aiding concept for low-altitude helicopter flight was developed and evaluated in a real-t...
Automated low-altitude flight and landing in remote areas within a civilian environment are investig...
In the last years UAV (Unmanned Aerial Vehicle) systems are become very actractive for various comme...
Work being accomplished to develop a real-time, piloted simulation of a helicopter using the vertica...
The ability to fly at low altitude while actively avoiding collisions with the terrain and objects s...
Helicopter flight is among the most demanding of all human-machine integrations. The inherent manual...
Abstract — Safe autonomous flight is essential for widespread acceptance of aircraft that must fly c...
NASA and the U.S. Army are jointly developing a teleoperated unmanned rotorcraft research platform a...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...