The parameter setting device has a parameter data input unit and a setting control unit which stores parameter data in an empty channel in the steering signal received from the transmitter and sends it to the transmitter. The parameter setting device and the transmitter are connected, and the parameter data is input to the parameter setting device. The parameter setting device stores the parameter data in the empty channel of the steering signal received from the transmitter and sends it back to the transmitter. The transmitter sends its steering signal to the body to be steered. The parameter data of the specific operation object mounted on the object to be steered can be reliably changed while continuing the operation of the operation object mounted on the object to be steered.

The Multi-Rotor Safety Shield (MRSS) provides a complete and substantial encasement system which can be secured about a Drone, protecting a multitude of aircraft components from contact with any outside disturbance and which can protect the sensitive components from dust, water, wind, rain, snow, fingers, toes, appendages of any kind, and atmospheric changes as example, from disabling the Drone and can protect people, places or things from high velocity spinning exposed rotor/propellers. The MRSS provides rigid non-permeable platform for attaching or incorporating additional safety devices as found in the Drone industry (or other industries) resulting in a safety device that completely prevents the loss a Drone due to the catastrophic failure of any Drone system or combination of systems which would typically result in rapid decent, and/or uncontrolled flight. The MRSS makes Drones safe near humans and safe to use around public gatherings, stadium events, accident scenes, disaster search and rescue and disaster relief, and indoors for the security and communications markets among others expanding the availability of Drones to further assist humanity.

A multi-layer, super-planar structure can be formed from distinctly patterned layers. The layers in the structure can include at least one rigid layer and at least one flexible layer; the rigid layer includes a plurality of rigid segments, and the flexible layer can extend between the rigid segments to serve as a joint. The layers are then stacked and bonded at selected locations to form a laminate structure with inter-layer bonds, and the laminate structure is flexed at the flexible layer between rigid segments to produce an expanded three-dimensional structure, wherein the layers are joined at the selected bonding locations and separated at other locations.

Disclosed is a motor bracket of a multicopter flying robot. The motor bracket for the multicopter flying robot disclosed in the present invention includes: a body 110 receiving a rotary motor 500 therein which is used in the multicopter flying robot, a connection portion 120 which is formed on the outer surface of the body and receives two power supply lines 510 and 520 connected to a power terminal of the rotary motor 500, and a power supply member 300 which is pushed into the connection portion 120 and electrically contacts the at least two power supply lines 510 and 520. The connection portion 120 includes a spatial separation portion 122 which performs a function of forming separated spaces of which the number is the same as the number of the at least two power supply lines 510 and 520.

There is provided a control device including an image display unit configured to acquire, from a flying body, an image captured by an imaging device provided in the flying body and to display the image, and a flight instruction generation unit configured to generate a flight instruction for the flying body based on content of an operation performed with respect to the image captured by the imaging device and displayed by the image display unit.

A toy vehicle includes a chassis, wheels connected to an exterior of the chassis and configured to move on a surface, at least two propellers connected to an interior of the chassis independently from the plurality of wheels, the at least two propellers being configured to counterrotate relative to each other thereby generating airflow outwardly from the chassis in a first direction that is normal to a rotational plane of the at least two propellers whereby the chassis is urged in a second direction opposite the first direction against the surface, at least one first drive motor operatively connected to the plurality of wheels for driving the plurality of wheels, and at least one second drive motor operatively connected to the at least two propellers for driving the at least two propellers.

A flying disc device appears to “flutter” in flight when rotating. The design is interesting and visually appealing when in use, is easy to see in flight, and can be easily retrieved when laying flat on the ground or another flat surface owing to its angularly oriented dual-disc design.

A flying disc device appears to “flutter” in flight when rotating. The design is interesting and visually appealing when in use, is easy to see in flight, and can be easily retrieved when laying flat on the ground or another flat surface owing to its angularly oriented dual-disc design.

A throwing and/or catching toy includes a generally elongated spheroidal body defining a longitudinal axis. A length of the body is longer than an equatorial diameter. A lift-generating wing is non-movably attached to the body near and/or at a center of the wing. At least one finger hold extension extends from a distal end of either a left or right wing portion. The finger hold extension is configured to allow a user to throw the toy in a discus-launched manner and the body is configured to be caught by the user. The lift-generating wing may be made as an injection molded, polymer wing. A manual adjuster may be associated with and controlling the shape of a horizontal stabilizer. A front end of the elongated body may be a resilient foam having a Shore A durometer hardness equal to or less than 25.

A control system for a vehicle using a primary three axis orientation sensor and a reference three axis orientation sensor spaced apart from the primary sensor. At least one auxiliary control can be used for thrust. A wearable processor can be configured to receive the primary sensor signal and the reference sensor signal. The reference sensor signal can use a conditioning formula and the wearable processor can filter the conditioned signals using a Kalman filter. The filtered signals can form merged signals and apply operator configurations on wrist reference locations to the merged signals. Operation commands can use the merged signals to control the vehicle with four channels of control to a transmitter that communicates with the vehicle.