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CONTRIBUTION TO THE DEVELOPMENT OF INERTIAL COORDINATORS FOR SHORT RANGE ROCKET MISSILES
Blizanac Borivoj
A possible form of inertial sensors and calculator elements configuration is described. Based on input data, coordinates of the center of gravity and angular rates components are calculated as an output as well as the angles of rotation of the dynamically coordinate system with respect to the geodesic coordinate system. There is a limit in the proposed method application, due to the adopted suggestion that the gravitational field acceleration direction is always parallel with the vertical axis of the geodesic coordinate system and that acceleration intensity has a constant value.
Ključne reči: Rocket missile, inertial coordinator, inertial sensor. |