Abstract: A detection unit directly detects an operating force acting on a wheel. A computation unit respectively computes a current value of a regenerative braking force and a current value of a friction braking force based on the result of a detection by the detection unit. A setting unit sets a target value of the regenerative braking force and a target value of the friction braking force based on a required braking force. A control unit controls a regenerative braking device based on the current value of the regenerative braking force so that the regenerative braking force approaches to the target value and also controls a friction braking device based on the current value of the friction braking force so that the friction braking force approaches to the target value.

Abstract: A landing-control device is provided having a new structure for carrying out landing control of an aircraft. A detecting unit 10 detects at least a relative altitude from a landing surface to an aircraft. A parameter-generating unit 20 is constructed by a neural network having a feedback loop which receives a detection value detected by the detecting unit 10 and outputs a landing-control parameter of the aircraft, an output of a first node among plural nodes constituting the neural network being input to a second node different from the first node. A controlling unit 30 controls the aircraft based on the control parameter output from the parameter-generating unit 20.

Abstract: A detection unit directly detects an operating force acting on a wheel. A computation unit respectively computes a current value of a regenerative braking force and a current value of a friction braking force based on the result of a detection by the detection unit. A setting unit sets a target value of the regenerative braking force and a target value of the friction braking force based on a required braking force. A control unit controls a regenerative braking device based on the current value of the regenerative braking force so that the regenerative braking force approaches to the target value and also controls a friction braking device based on the current value of the friction braking force so that the friction braking force approaches to the target value.

Abstract: A landing-control device is provided having a new structure for carrying out landing control of an aircraft. A detecting unit 10 detects at least a relative altitude from a landing surface to an aircraft. A parameter-generating unit 20 is constructed by a neural network having a feedback loop which receives a detection value detected by the detecting unit 10 and outputs a landing-control parameter of the aircraft, an output of a first node among plural nodes constituting the neural network being input to a second node different from the first node. A controlling unit 30 controls the aircraft based on the control parameter output from the parameter-generating unit 20.