| 摘要 |
FIELD: aviation.SUBSTANCE: invention relates to navigation systems and can be used in rocketry. Aircraft missile (AM) with inertial navigation system with possibility to rotate includes gyroscopic sensor of pitch angular speed, automatic control system with automatic control facilities. AM is automatically turned about its longitudinal axis, after each AM turn around its axis direction of rotation is changed, eliminating effect of pitch angular speed gyroscopic sensor scaling factor, and drifts are corrected.EFFECT: invention makes it possible to replace gyroscope with pitch angular speed gyroscopic sensor in inertial navigation systems.4 cl, 3 dwg |
