62 results about "Flight pattern" patented technology

The present invention relates to a system for retrieving data from remote difficult to reach terrain, such as wilderness areas, etc. and in particular to a system comprised of one or more surface based data collectors in communication with one or more wireless transceivers adapted to transmit the collected data to an unmanned aerial vehicle adapted to fly within a predetermined distance from the data collector and receive data collected therefrom. The present invention further relates to an unmanned aerial vehicle adapted to fly a flight pattern relative to a moveable surface object or for controlling the position of a moveable surface object relative to the flight path of the unmanned aerial vehicle. Finally, the present invention relates to an improved unmanned aerial vehicle having airframe structural elements with electrical circuits adhered to the surfaces of the structural elements.

An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.

An improved golf ball driver has a first weight positioned within the clubhead of the driver, and a first means for adjusting the first weight in a generally vertical direction within the clubhead, that is, from top to bottom thereof. The improved driver also has a second weight positioned within the clubhead, and a second means for adjusting the second weight in a generally horizontal direction within the clubhead, that is from the heel to the toe thereof. Adjusting the weights allows a golfer to eliminate natural swing problems and/or to make a desired change in the flight pattern of a golf ball when it is struck by the driver.

A system and method for deploying and/or retrieving a cable underwater. In an embodiment, a system comprises a cage, comprising a guidance system adapted to be remotely operable subsea by a vessel; a communications link operatively linking the guidance system and the vessel; and a non-palletized reel rotatably and removably mounted within the cage, the reel adapted to receive an unspoolable length of cable, the cable comprising two fee ends. In an exemplary method, the reel, onto which cable is spooled is removably and rotatably housed in a cage adapted for remote control use underwater and the cage lowered by a vessel to a position proximate a seafloor. The cage is maneuvered along a predefined flight pattern in substantially a single plane with respect to the seafloor while selectively releasing the cable from the reel. It is emphasized that this abstract is provided to comply with the rules requiring an abstract which will allow a searcher or other reader to quickly ascertain the subject matter of the technical disclosure. It is submitted with the understanding that it will not be used to interpret or limit the scope of meaning of the claims.

An aircraft-mounted base transceiver station (mBTS) for providing intermittent coverage in a cellular radio network. The mBTS utilizes the existing protocol of its terrestrial counterparts, thereby avoiding dual-mode devices and enabling common usage of terminal monitoring and device management systems for devices connected to a single radio access network even when outside terrestrial coverage areas. The aircraft follows a transient flight pattern, providing intermittent flyover connectivity for remote radio device such as machine-type devices. Connectivity may be store and forward. Channel usage may be adjusted to avoid interfering with terrestrial communication cells during flyover. Doppler effects due to aircraft speed may be accounted for. The mBTS may be configured to service in-range radio devices which are outside a Doppler-inhibited region and/or to prioritize communication with devices based on expected time outside the Doppler-inhibited region. An aircraft mounted antenna may have a radiation pattern focused toward devices outside the Doppler-inhibited region.

A system and method for autonomous dynamic air traffic management. The method includes sensing a current location of a flying platform using at least one of a plurality of positioning sensors onboard the flying platform, transmitting location transmissions and receiving location transmissions from other flying platforms, determining from the received location transmissions and the sensed current location whether the flying platform and another flying platform are flying in a mutually intentional flight pattern or in a mutually unintentional flight pattern, based on one or more indications; refraining from alerting when the flying platform and the other flying platform fly close to each other within a predetermined range when flying in a mutually intentional flight pattern; detecting a risk of collision between the flying platform and said another of said one or a plurality of flying platforms; and generating an evading action instruction for the flying platform to avoid the collision.

Method and system for analyzing aircraft data, including multiple selected flight parameters for a selected phase of a selected flight, and for determining when the selected phase of the selected flight is atypical, when compared with corresponding data for the same phase for other similar flights. A flight signature is computed using continuous-valued and discrete-valued flight parameters for the selected flight parameters and is optionally compared with a statistical distribution of other observed flight signatures, yielding atypicality scores for the same phase for other similar flights. A cluster analysis is optionally applied to the flight signatures to define an optimal collection of clusters. A level of atypicality for a selected flight is estimated, based upon an index associated with the cluster analysis.

Described herein are systems and methods for tracking suspect aircraft. One embodiment is related to a method including receiving location data and current flight data of an aircraft, analyzing the location data and current flight data using flight behavior algorithms, detecting route deviation of the aircraft, and providing a report of flight pattern analysis and the detected route deviation to at least one device on a network. Another embodiment is related to a system comprising a location network determining location data of an aircraft, a searchable database storing historical flight activity data, current flight data, and the location data from the location network, a flight tracking module receiving location data and the current flight data of the aircraft from the database, analyzing the location data and current flight data using flight behavior algorithms, detecting route deviation of the aircraft based on the historical flight activity data, and providing a report of flight pattern analysis and the detected route deviation to at least one device on a network.

The disclosure provides an approach for performing inspections. An image analysis application is configured to receive sensor data captured at least by one or more sensors mounted on a first unmanned aerial vehicle (UAV) flying along at least one programmed flight pattern. The image analysis application is further configured to normalize the sensor data, and determine anomalies based, at least in part, on differences between the normalized sensor data and sensor data previously captured at least by one or more sensors mounted on a second UAV flying along the at least one programmed flight pattern. In addition, the image analysis application is configured to generate a report indicating the determined anomalies.

A bistatic radar system and method. In the illustrative embodiment, a receiver is positioned in a horizontal plane. A transmitter is then positioned in Middle Earth Orbit at a position that is nearly vertical to the plane of the receiver. This configuration provides significant flexibility for the radar system. As such, the radar system may engage in flight patterns, in which the transmitter and receiver have velocity vectors in opposite directions (GMTI mode), the same direction (SAR mode) and variations in between (mixed mode). Lastly, a broad beam is generated from the transmitter and illuminates an area enabling several receivers to simultaneously observe the illuminated area.

An aircraft includes a fuselage, a wing, a ducted fan and a controller. The wing and the ducted fan are coupled to the fuselage. The controller is operable to control the aircraft in a vertical flight mode, a horizontal flight more, and transition the aircraft from the vertical flight mode to the horizontal flight mode.

A communication system for supporting communications with a target market area. The system includes one or more solar-powered aircraft maintained in, or successively passing through, flight stations or flight patterns around the market area. Each of the aircraft targets limited beamwidth communication antennas on a substantial portion of the target market area. The control system is configured to fly selective flight patterns depending on the aircraft characteristics and the flight conditions. The flight patterns may emphasize high-power-generation patterns such as flying away from the sun for aircraft with wing-mounted solar cells.

This waterfowl decoy kite is designed in a manner that allows for its deployment over a body of water or other potential waterfowl landing area to facilitate the attracting of specific species to the hunter. The kite is made from a an oval wing and circular stabilizer. The wing and stabilizer may have a variety of notches so as to impart bird like characteristics to the kites flight pattern and visual appeal. The kite may also be painted so as to exhibit a bird like appearance during flight.

A kite for a system for extracting energy from the wind, the kite comprising: a body having a wing for providing lift; means for connecting the wing to a tether; and means for controlling the flight of the kite in the wind, wherein the wing is constructed with an asymmetry in a spanwise direction from a first end of the wing to a second end of the wing to provide the wing with a naturally asymmetric shape at least when in flight. The asymmetry may be provided to optimise the shape of the wing for a flight pattern in which one end of the wing has a higher speed than the other end of the wing. For example, the asymmetry may be optimised to allow the kite to follow a flight pattern resembling a circle or spiral, from the point of view of a base unit of the system.

A substantially cup-shaped throwing and hitting sports toy is provided having a flared open end portion, a body portion, and a closed end portion. The structure of the toy provides for various flight patterns while being suitable for use in limited areas of space.

The invention provides a flight state information displaying method of an unmanned aerial vehicle. The flight state information displaying method comprises the steps of obtaining all flight state information of the unmanned aerial vehicle, determining flight modes of the unmanned aerial vehicle according to the flight state information of the unmanned aerial vehicle, selecting relevant flight state information associated with the flight modes of the unmanned aerial vehicle from all the flight state information and displaying the relevant flight state information on a display screen of a remote-control unit of the unmanned aerial vehicle. The invention further provides a flight state information displaying device of the unmanned aerial vehicle. The flight state information displaying method and the flight state information displaying device of the unmanned aerial vehicle determine the relevant flight state information displayed on the display screen according to the flight modes of the unmanned aerial vehicle so that a user can obtain the flight states of the unmanned aerial vehicle in time and can accurately control the unmanned aerial vehicle.