8th AIAA Atmospheric and Space Environments Conference 2016
DOI: 10.2514/6.2016-3584
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Fundamental Turbulence Measurement with Unmanned Aerial Vehicles (Invited)

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Cited by 6 publications
(9 citation statements)
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“…Data evaluation, reduction and ABL characterization analyses are conducted by the various sub-task contributors (See Figure 6). Witte, for example, developed a fixed-wing sUAS sensing platform and data reduction to measure and characterize ABL turbulence and validated its performance in comparison to measurements from vertical profiles of a rotary-wing platform, and a portable tower-based sonic anemometer [17].…”
Section: And 2017 Cloud-map Flight Campaign Overviewmentioning
confidence: 99%
“…Data evaluation, reduction and ABL characterization analyses are conducted by the various sub-task contributors (See Figure 6). Witte, for example, developed a fixed-wing sUAS sensing platform and data reduction to measure and characterize ABL turbulence and validated its performance in comparison to measurements from vertical profiles of a rotary-wing platform, and a portable tower-based sonic anemometer [17].…”
Section: And 2017 Cloud-map Flight Campaign Overviewmentioning
confidence: 99%
“…During these studies, the probe tubing length was optimized to provide a fre-quency response on the order of 100 Hz. At the typical cruise speed of BLUECAT5, this frequency response translates to a spatial measurement resolution of approximately 0.2 m. Additional wind and water tunnel studies verified that positioning the measurement volume of the probe 18 cm upstream of the nose of the aircraft was sufficient to minimize interference effects from the airframe (Witte et al, 2017).…”
Section: Bluecat5 Uasmentioning
confidence: 85%
“…1a, were constructed from Skywalker X8 airframes, modified to introduce semiautonomous operation by integrating a 3DR Pixhawk autopilot, and ruggedized by strengthening wing spars, skinning the aircraft, adding Kevlar landing skids, and shielding to minimize the ingestion of dirt into the motor. Referred to as the Boundary Layer Unmanned Experiment for the Characterization of Atmospheric Turbulence generation five (BLUECAT5) UASs (Witte et al, 2017), the aircraft had endurance of up to 45 min with 20 m s −1 cruise speeds and were catapult launched and skid landed. The four aircraft used here are identified as BCT5B, BCT5C, BCT5D and BCT5E.…”
Section: Bluecat5 Uasmentioning
confidence: 99%
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“…Qu, Xing, & Zhang (2016) used a decomposition of the hovering state equations to estimate the wind, and Qu, Xing, Zhang, & Yu (2017) extended the work using both IMU and a smoothing filter to reduce the effect of sensor noise. Witte et al (2016) used a method based on on-board moving velocity sensors data such as five-hole and hot-wire probes. Benallegue, Mokhtari, & Fridman (2008) built the high-order sliding mode observer as an estimator of the effect of the external disturbances in quadrotors such as wind and noise, using a differential global positioning system, a GPS, and a sonar altimeter.…”
Section: Introductionmentioning
confidence: 99%