Method and relative angular position control apparatus by vibrant structure girometer, with absolute position correction through control beacon, for maintenance, entertainment and simulation systems of short-scope lanzamisil platforms. (Machine-translation by Google Translate, not legally binding)

摘要

Method and angular position control device for a system with two axes of rotation to be used with a computerized microprocessor system, for the continuous detection of the angular position of a system with two axes of rotation by gyrometers of vibrating structure, with automatic correction of the deviations in the measurement by comparison with data obtained from the position of a fixed external reference beacon. More particularly, the invention relates to angular position control for maintenance, training and simulation systems of short range missile launch platforms, and equivalent equipment, provided that their movements have the two degrees of freedom of azimuth and elevation. The control method and apparatus, by its nature of universal application with inertial sensors, allows its application in multiple platforms regardless of the sensor system of these, or even in those cases in which they do not include angular sensors. The method and control device, by its automatic correction form, allows the use in multiple simultaneous systems, with a common reference to all of them, so that they are synchronized. These systems can be homogeneous or heterogeneous. (Machine-translation by Google Translate, not legally binding)