A flight control system for an aircraft receives a selected value of a first parameter, which is either the airspeed or inertial velocity of the aircraft.
Techniques are provided for reducing mount vibration in an inertial rate sensor (IRS).
According to the invention, the position where the other vehicle is level with one's own vehicle is determined on the basis of the inertial speed vector of the other vehicle (25) at one or more points in time.
A vibrating inertial rate sensor has operational elements that define axes that are rotationally offset or 'skewed' from a node or anti-node reference axis.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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