METHOD OF INERTIAL NAVIGATION AND DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2008 - IPC G01C21/16 G01P15/08 

FIELD: physics; transportation.

SUBSTANCE: method of inertial navigation consists in application of self-oscillation linear accelerometers, by indications of which: Δn_i=n_1i-n_2i, n_i=n_1i+n_2i=f_cT_i and N_ai=Δn_i/n_i=K_aia_i, (i=1...∞), proportional to acceleration and self-oscillation period T_i, where K_ai=ml/K_tsI₀ is accelerometer transformation coefficient, ml is pendulous braking of accelerometer moving system, K_ts and I₀ is torque sensor transfer constant and current supplied by stabilised source; simultaneously with object acceleration time interval n_i=f_cT_i is measure to measure acceleration, by accelerometer indications the components of velocity vector and of radius vector in direction of accelerometer sensitivity axis within this interval. To detect components of velocity vector N_vi and of radius vector N_ri the accelerometer values N_ai and n_i for each self-oscillation T_i are multiplied and results of certain path segment are added.

EFFECT: reduced time of navigation data preparation and reduced number of applied means due to expansion of linear accelerometer functionality.

2 cl, 1 dwg