Abstract:
An actual position of a load tethered with a tether to a vehicle is determined using a plurality of sensors disposed on the vehicle. A required tether tension and required tether angle of the tether is determined to move the load from the actual position to a commanded position. An actual tether tension and actual tether angle of the tether is determined using the plurality of sensors. A determination is made as to a thrust vector to be applied by the vehicle to change the actual tether tension and the actual tether angle of the tether to the required tether tension and the required tether angle. The thrust vector is applied with the vehicle to reposition the vehicle to achieve the required tether angle and to create the required tether tension of the tether to move the load to the commanded position.
Abstract:
Disclosed herein are example embodiments for base station multi-vehicle coordination. For certain example embodiments, at least one machine, such as a base station, may: (i) effectuate one or more communications with at least a first UFV and a second UFV; or (ii) transmit to a first UFV at least one command based at least partially on one or more communications with at least a first UFV and a second UFV. However, claimed subject matter is not limited to any particular described embodiments, implementations, examples, or so forth.
Abstract:
A method for controlling a swarm of autonomous vehicles to perform a multitude of tasks using either a one touch or a single gesture/action command. These commands may include sending the swarm on an escort mission, protecting a convoy, distributed surveillance, search and rescue, returning to a base, or general travel to a point as a swarm. A gesture to initiate a command may include a simple touch of a button, drawing a shape on the screen, a voice command, shaking the unit, or pressing a physical button on or attached to the mobile platform.
Abstract:
Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.