| 摘要 |
<p>The method involves measuring vector components of speed (v) of a missile (1) along the axes periodically using a global positioning system (GPS) (9). Vector components of the missile acceleration (gamma ) are evaluated from the measurements. Values of Euler angles of the missile are recalculated by combining the speed (V), acceleration (gamma ) and the missile acceleration measured by an inertial unit (10).</p> |
