Dorozhkkin А.D. 1
Dzhus О.А. 1
1 FGKU VPO “Military Academy of Aerospace Defense named after Marshal Zhukov”
In existing inertial navigation systems (INS) is a significant increase of position errors of the aircraft (LA) in time because of instrumental errors. This fact does not allow to achieve high efficiency of combat actions without the implementation of the periodic adjustment of ins, usually using positional navigation systems (RSBN, RSDN). Association navigation devices and individual systems in flight and navigation complex (NCP) and the sharing of their information has allowed to increase accuracy and reliability of data on parameters of movement and system status. One of the most difficult operating modes, the NCP is a correction mode, during which involved almost all the NCP s ystem and links between them. The analysis of efficiency of methods of increase of accuracy with respect to inertial navigation systems (ins). As they have the features of the autonomy, noise immunity, secrecy of work, are the main and most complex springs flight and navigation information in modern NCP. The conclusion is that the perspective is the application of the scheme wave solid-state gyroscopes (VTG) in the general structure of the NCP.