A waterfowl decoy apparatus comprising a vertical shaft, a hinging mechanism that is movable between a deployed position and a closed position mechanically connected to the vertical shaft, a windsock support structural member having a first end pivotally connected to the hinging mechanism and a windsock slidably connected to the windsock support structural member. When the hinging mechanism is in the deployed position, the windsock support structural member and the windsock is perpendicular to the vertical shaft. When the hinging mechanism is in the closed position, the windsock support structural member and windsock is parallel to the vertical shaft.

Systems and methods for detecting touch events with an accelerometer are disclosed. In one aspect, a method includes measuring first accelerometer data at a first rate, detecting a first touch event based on the first accelerometer data, in response to detecting the first touch event, measuring second accelerometer data at a second rate, determining whether a second touch event is detected based on the second accelerometer data, measuring third accelerometer data at the first rate in response to an absence of the second touch event being detecting in the second accelerometer data over a predetermined threshold period of time.

Embodiments of methods and apparatus for close formation flight are provided herein. In some embodiments, an apparatus for close formation flight, comprises a plurality of sensors for collecting measurements characterizing airflow near an aircraft. The plurality of sensors are attachable to at least one of a wing, fuselage, or tail of the aircraft, and the measurements provide information about airflow velocity in a direction transverse to a direction of the aircraft flight.

A system for displaying information obtained along the direction of flight of an aircraft is provided. The system includes a vane assembly pivotally mounted to the aircraft having a sensor mounted thereto. The vane comprises a pointing axis configured to continuously align with the direction of the flight path of the aircraft. A display device is operatively connected to the output of the sensor for providing a display along the actual flight path of the aircraft.

A method for calibrating a wind direction measurement for a wind turbine is provided. The method including: measuring plural samples of a relative wind direction representing a difference angle between a real wind direction and an orientation of a measurement equipment, in particular a direction orthogonal to a rotor blade plane, to obtain plural measured relative wind directions; deriving a measured relative wind direction change based on the measured relative wind directions; measuring plural samples of a performance parameter indicating a performance of the wind turbine; deriving a performance change based on the plural samples of the performance parameter; determining a correlation value between the measured relative wind direction change and the performance change; measuring further plural samples of the relative wind direction; and correcting the further measured relative wind directions based on the correlation value, to obtain corrected further measured relative wind directions.

A method for calibrating a wind direction measurement for a wind turbine is provided. The method including: measuring plural samples of a relative wind direction representing a difference angle between a real wind direction and an orientation of a measurement equipment, in particular a direction orthogonal to a rotor blade plane, to obtain plural measured relative wind directions; deriving a measured relative wind direction change based on the measured relative wind directions; measuring plural samples of a performance parameter indicating a performance of the wind turbine; deriving a performance change based on the plural samples of the performance parameter; determining a correlation value between the measured relative wind direction change and the performance change; measuring further plural samples of the relative wind direction; and correcting the further measured relative wind directions based on the correlation value, to obtain corrected further measured relative wind directions.

In an embodiment, a method for aircraft weight estimation is provided that includes determining a weight signal based on a dynamic pressure signal, a calibrated angle of attack signal, a lift coefficient signal, a load factor signal, and a wing surface area. In another embodiment, a method to estimate aircraft weight is provided that includes determining a weight based on historical flight data relating horizontal control surface position to dynamic pressure. In another embodiment, a system for continuously estimating aircraft weight during flight is provided that includes a pitot-static subsystem, an angle of attack indicator, an accelerometer, a controller configured to provide a weight signal, and a signal filter for filtering the weight signal to determine a stable aircraft weight.

An independently operable flight data capture and transmission device includes an aerodynamically efficient main body having a mounting bracket for securing the device onto the wings, fuselage or strut of an aircraft during flight. A sensor suite is positioned within the main body to independently capture flight data information pertaining to the flight characteristics, statistics, metrics, performance and environment of the aircraft during flight. A control unit is positioned within the main body to selectively control an operation of the sensor suite, store the flight data information within a memory and communicate with a user device. A mobile application displays the flight data information and communicates operating instructions to the device, and a power generation unit generates power for use by the system components during flight.

A wind sensor has a housing and a wind detection element, which is rotatably mounted on the housing and is formed by a wind wheel having a cup-star including a plurality of cups, wherein at least one ohmic heating element is incorporated in the wind wheel. Structures are provided for transferring energy between the housing and the ohmic heating element rotating with the wind wheel. The structures can include a primary coil arranged in the housing and a secondary coil arranged in the wind wheel, wherein the secondary coil is connected to the ohmic heating element. The plurality of cups of the wind wheel are each mounted by way of flat webs, wherein the webs extend into the cups and divide the cups into two regions, and the at least one heating element is embedded in the webs and extends into the region of the cups.

A wind sensor has a housing and a wind detection element, which is rotatably mounted on the housing and is formed by a wind wheel having a cup-star including a plurality of cups, wherein at least one ohmic heating element is incorporated in the wind wheel. Structures are provided for transferring energy between the housing and the ohmic heating element rotating with the wind wheel. The structures can include a primary coil arranged in the housing and a secondary coil arranged in the wind wheel, wherein the secondary coil is connected to the ohmic heating element. The plurality of cups of the wind wheel are each mounted by way of flat webs, wherein the webs extend into the cups and divide the cups into two regions, and the at least one heating element is embedded in the webs and extends into the region of the cups.