| 摘要 |
FIELD: aviation. ^ SUBSTANCE: invention relates to vertical-plane guidance final approach instrument. The proposed device incorporates navigation system to determine final approach trajectory, inertial reference system to prepare inertial data on aircraft location and to prepare hybrid location of aforesaid aircraft, multi-mode receiver to facilitate final approach which receives the data on flight trajectory and hydrid location. Aforesaid receiver derives, from aforesaid data, lateral and vertical angular deviations with final approach axis locked-on. The proposed device incorporates also the navigation system to receive aforesaid vertical and lateral angular deviations to be used for aircraft guidance. Note here that aforesaid multi-mode receiver incorporates integrated monitoring system to track operating parametres related to location obtained of the basis of aforesaid various data by inertial reference system. ^ EFFECT: facilitating aircraft instrumental vertical-plane guidance final approach. ^ 7 cl, 1 dwg |
