ADJUSTABLE SINGLE-CHANNEL INERTIAL NAVIGATION SYSTEM WITH NORTHERN SIDE CHANNEL

摘要

The invention applies to aircraft's navigation industry. It gives possibility to decrease mistakes of the inertial navigation system and to accomplish inertial system technically more simple. The developed inertial navigation system which funkcional fow chart is shown in Fig.2 consists of one north-channel and two dynamic chains. In the dynamic chains occurs counting of the east velocity and the side velocities elements. In the north-channel the north directions parameters are being counted, as well as width angles quantity. The developed single-channel inertial system contains specific correction chains that substantially decrease system's failures. The correction chain receives the information from side devices - speed device and heading system. The developed single-channel north-side inertial navigation system can be used in the military and civil aviation. In the civil aviation single-channel adjustable north-side inertial system may be used in relatively small aircrafts. On its basis pilotage and navigation complex might be made. In the military aviation single-channel adjustable north-side inertial system can be used in pilotless aircrafts in automatic control system contour. That gives possibility to fulfill the aircrafts self-governing (dormant) flight.