Abstract: The invention concerns a device (1) comprising means (6A, 6B, 6n) which determine for each of the engines of the aircraft, an individual minimum flexible temperature and means (8) which determine a global minimum flexible temperature based on said individual minimum temperatures, enabling a maximum available thrust to be calculated.
Abstract: The present invention provides a technique that makes a robot continue a stabilized walk, even when an actual movement state of the robot deviates greatly from a target movement state of the robot. The robot includes a trunk, a pair of leg links coupled with the trunk in a swingable manner, an actuator group that swings each of the leg links independently to the trunk, and a controller that controls the actuator group. The controller is programmed to control the actuator group and realize a given trajectory of the center of gravity and the trajectory of the toe of the leg link.