The invention relates to techniques for verifying a nacelle yaw position sensor installed on a wind turbine and for taking restorative action to control the nacelle yaw position. The invention relates to a method performing the comprising determining a first absolute wind direction signal associated with the first wind turbine; determining a second absolute wind signal direction signal associated with the plurality of other wind turbines; comparing the two wind direction signals; and issuing a nacelle yaw position sensor fault signal if the first signal is beyond a predetermined error range of the second signal. A benefit of the invention is that it enables the detection of an inaccurate nacelle yaw sensor without direct measurement or inspection.

The invention relates to techniques for verifying a nacelle yaw position sensor installed on a wind turbine and for taking restorative action to control the nacelle yaw position. The invention relates to a method performing the comprising determining a first absolute wind direction signal associated with the first wind turbine; determining a second absolute wind signal direction signal associated with the plurality of other wind turbines; comparing the two wind direction signals; and issuing a nacelle yaw position sensor fault signal if the first signal is beyond a predetermined error range of the second signal. A benefit of the invention is that it enables the detection of an inaccurate nacelle yaw sensor without direct measurement or inspection.

A method for calculating a true wind direction and a true wind speed by adjusting measured values of an anemometer mounted on a vehicle based on observation errors caused by a degree of slant of the vehicle and a device using the same are provided. The method includes steps of: (I) acquiring a Gt, which is information on the degree of slant corresponding to a current time t, from an electronic compass module, and (II) acquiring a Wmt which is information on a measured wind measured by the anemometer at the current time t, to acquire a Wmt′, which is information on a measured corrected wind in a space after a first error correction on the Wmt by referring to the Gt, to thereby calculate a first true wind direction and a first true wind speed.

A method for manufacturing a tower structure of a wind turbine at a wind turbine site. The method includes determining an optimized shape of the tower structure based on one or more site parameters. Further, the optimized shape of the tower structure is non-symmetrical. In a further step, the method include printing, via an additive printing device, the optimized shape of the tower structure of the wind turbine at the wind turbine site, at least in part, of a cementitious material. In addition, the method includes allowing the cementitious material to cure so as to form the tower structure of the wind turbine.

Systems and methods for predicting aircraft navigation performance are provided. In one embodiment, a method can include determining that one or more navigational aid measurements are not available to the aircraft. The method can include estimating a future actual navigation performance of the aircraft for a future point in the flight plan. The method can include determining a future required navigation performance associated with the future point in the flight plan. The method can include comparing the future actual navigation performance to the future required navigation performance to determine if the future actual navigation performance satisfies the future required navigation performance. The method can include providing, to an onboard system of the aircraft, information indicative of whether the future actual navigation performance satisfies the future required navigation performance.

Method and apparatus are disclosed for preventing damage to an object within a charging field of a wireless vehicle battery charger. An example vehicle includes a wireless vehicle battery charger having a charging field, a plurality of Bluetooth antennas, and a processor. The processor is configured to identify a location of an object using one or more of the plurality of Bluetooth antennas, and, responsive to determining that the object is within the charging field, disable the wireless vehicle battery charger.

A method, apparatus, and computer program product for identifying air data for an aircraft. The lift for the aircraft is identified. The number of surface positions for the aircraft is identified. The angle of attack during flight of the aircraft is identified. A synthetic dynamic pressure is computed from the lift, the number of surface positions, and the angle of attack.

Methods, apparatuses, and systems for air sampling and emissions monitoring based on wind direction, including determining concentrations of air toxics, are contemplated. Some embodiments comprise detecting wind flowing in a first direction and a second direction, exposing a sample collection device to air in response to detecting the first direction and preventing exposure of the sample collection device to air in response to the second direction. Some apparatuses comprise a direction detector, an enclosure, and a sample preventer. Some embodiments comprise a purger configured to purge the sample collection device when preventing exposure of the sample collection device to air. In some embodiments, the sample collection device comprises a diffusive sorbent tube. In some embodiments, the diffusive sorbent tube is configured to collect samples of benzene. Some embodiments comprise a wind vane and sensor configured to provide indication of wind direction. Some embodiments comprise a data collector.

Methods, apparatuses, and systems for air sampling and emissions monitoring based on wind direction, including determining concentrations of air toxics, are contemplated. Some embodiments comprise detecting wind flowing in a first direction and a second direction, exposing a sample collection device to air in response to detecting the first direction and preventing exposure of the sample collection device to air in response to the second direction. Some apparatuses comprise a direction detector, an enclosure, and a sample preventer. Some embodiments comprise a purger configured to purge the sample collection device when preventing exposure of the sample collection device to air. In some embodiments, the sample collection device comprises a diffusive sorbent tube. In some embodiments, the diffusive sorbent tube is configured to collect samples of benzene. Some embodiments comprise a wind vane and sensor configured to provide indication of wind direction. Some embodiments comprise a data collector.

Air data sensing apparatus comprising: an aircraft panel; a blister arranged on a surface of the aircraft panel, the blister comprising an upstream portion and a downstream portion, the upstream portion being rounded in three dimensions and having a rounded outer edge surface spaced laterally from the aircraft panel; a plurality of apertures in the surface of the aircraft panel, the apertures being adjacent to the upstream portion of the blister, and spaced from the blister; a plurality of conduits, each conduit being in fluid communication with a respective aperture; and one or more pressure sensors arranged to measure a pressure in each of the conduits.