A method for determining a state of credibility of measurements made by sensors of an aircraft is provided. This method includes determining a speed of the aircraft, from static and total pressure measurements, determining a coefficient of lift of the aircraft from an incidence measurement and from said speed, determining a weight of the aircraft, determining if an equation of lift of the aircraft is satisfied, activating a state of optimal credibility, wherein the measurements made by said sensors are considered to be reliable if the said equation of lift is satisfied, activating a state of non-optimal credibility, wherein the measurements of at least one sensor are considered to be unreliable if the said equation of lift is not satisfied.

A motorcycle has a video camera attached thereto in such a manner as to shoot sharp images. A motorcycle includes a camera adapted to shoot a road surface. The camera is arranged below an engine or a swing arm and more rearward than the center of a crankshaft of the engine. The swing arm pivotally supports a rear wheel with a rear edge portion thereof. The camera is fastened to, and supported either by a lower portion of the engine or by a lower portion of a vehicle body frame connected to the engine.

A method for calculating a scale factor for a gyroscope can include detecting, by a gyroscope, a physical motion of a robot, detecting, by an optical flow (OF) sensor (and/or camera), one or more image signals including information; and deriving estimates of sensor calibration parameters based on the detected physical motion and the information.