Abstract: A power wheel including a positioning device, a wireless communication module, and a controller is provided, where the controller is configured to operate in an active mode or a passive mode. When operating in the passive mode, the controller is configured to: acquire route information and moving information from the power wheel operating in the active mode by the wireless communication module, and acquire relative position information with the other power wheels by the positioning device; and determine a rotation strategy of the power wheel according to the route information, the moving information and the relative position information. When operating in the active mode, the controller is configured to: acquire the route information, and transmit the route information to the other power wheels; and determine the rotation strategy of the power wheel according to the route information. In addition, a cooperative carrying method of the power wheel is also provided.

Abstract: A power wheel including a positioning device, a wireless communication module, and a controller is provided, where the controller is configured to operate in an active mode or a passive mode. When operating in the passive mode, the controller is configured to: acquire route information and moving information from the power wheel operating in the active mode by the wireless communication module, and acquire relative position information with the other power wheels by the positioning device; and determine a rotation strategy of the power wheel according to the route information, the moving information and the relative position information. When operating in the active mode, the controller is configured to: acquire the route information, and transmit the route information to the other power wheels; and determine the rotation strategy of the power wheel according to the route information. In addition, a cooperative carrying method of the power wheel is also provided.

Abstract: An error correcting method is provided, which includes the following steps. An error value is obtained. The error value is substituted into an error correcting function, so that the error correcting function causes the error value to converge to 0 in a finite time. The error correcting function conforms to a non-Lipschitzian characteristic. An embodiment of the disclosure solves the problem in traditional system stability analysis through a differential equation, adjusts parameters to determine a convergence time, and ensures that a convergence target fully conforms to an expected value and that a unique solution of the error value is 0.

Abstract: An amorphous alloy material is provided, including 55%˜65% iron, 10%˜20% cobalt, 13%˜17% silicon, 8%˜12% boron and unavoidable impurity in weight percentage. The amorphous alloy material has good soft magnetic performance.

Abstract: An electromagnetic thermotherapy estimation system adapted to estimate an ablation result of a biological tissue ablated by a needle induced by an electromagnetic coil is provided. The electromagnetic thermotherapy estimation system includes an input device and a processing device. The input device is configured to receive a plurality of setting parameters. The setting parameters include a needle tip depth and a current magnitude. The processing device is electrically connected to the input device, and has a database configured to store an ablation range estimation model and a temperature envelope estimation model. The processing device is configured to calculate ablation range data and temperature envelope data corresponding to the setting parameters according to the ablation range estimation model, the temperature envelope estimation model and the setting parameters. In addition, an electromagnetic thermotherapy estimation method is also provided.

Abstract: A multiple rotors aircraft and a control method thereof are provided. The control method comprises the following steps. First, current motion information of the multiple rotors aircraft is obtained. Then, at least one control gain is adjusted through a gain adjustment function according to the current motion information. The gain adjustment function conforms to a non-Lipschitzian characteristic, and at least one rotor of the multiple rotors aircraft is controlled according to the control gain. Therefore, the multiple rotors aircraft would be ensured that its flight attitude is toward a target position, and the expected result would be conformed rapidly.

Abstract: An information backing up method and system are provided. The information backing up system at least includes a moving vehicle and a server. The moving vehicle obtains its external information and internal information, establishes a transmitting connection with the server through a machine-to-machine (M2M) protocol, and transmits the external information and the internal information to the server through the transmitting connection. In addition, the information backing up system may further include a network gateway device, so that the moving vehicle can perform an information backup procedure through the network gateway device.

Abstract: An error correcting method is provided, which includes the following steps. An error value is obtained. The error value is substituted into an error correcting function, so that the error correcting function causes the error value to converge to 0 in a finite time. The error correcting function conforms to a non-Lipschitzian characteristic. An embodiment of the disclosure solves the problem in traditional system stability analysis through a differential equation, adjusts parameters to detei nine a convergence time, and ensures that a convergence target fully conforms to an expected value and that a unique solution of the error value is 0.

Abstract: An additive manufacturing method is provided. A plurality of powder layers is stacked on a supporting plate in sequence. Energy beams are provided to the powder layers in sequence by using an energy source, such that each of the powder layers is at least partially shaped. The powder layers are heated by using a temperature control device, so as to control a temperature of each of the powder layers being shaped.

Abstract: An additive manufacturing apparatus including a supporting plate, an energy source and a temperature control device is provided. A plurality of powder layers are adapted to be stacked on the supporting plate in sequence. The energy source is adapted to provide energy beams to the powder layers in sequence, such that each of the powder layers is at least partially shaped. The temperature control device is adapted to heat the power layers, so as to control a temperature of each of the powder layers being shaped.

Abstract: A multiple rotors aircraft and a control method thereof are provided. The control method comprises the following steps. First, current motion information of the multiple rotors aircraft is obtained. Then, at least one control gain is adjusted through a gain adjustment function according to the current motion information. The gain adjustment function conforms to a non-Lipschitzian characteristic, and at least one rotor of the multiple rotors aircraft is controlled according to the control gain. Therefore, the multiple rotors aircraft would be ensured that its flight attitude is toward a target position, and the expected result would be conformed rapidly.