FIELD: military equipment.
SUBSTANCE: invention relates to military equipment and can be used for aiming cruise missiles (CM) mounted on self-propelled launcher. In order to aim cruise missiles on self-propelled launcher (SPL), azimuth angle of inertial unit (IU) of missile is determined by known azimuthal angle of routing-navigation system of surveying and orientation (RNSSO) of self-propelled launcher. At that, during standard electric checks at horizontal position of lifting boom with rockets and RNSSO, angular mismatch is measured by roll between inertial rocket unit and RNSSO and after the SPL boom is moved to the vertical start position, the measurement results are used to calculate the correction to the azimuth angle measured by the RNSSO. Provided is fewer measurements and initial IU CM in prelaunch preparation not only in horizontal position CM on SPL, but in vertical, which increases accuracy of determination of mutual position of axes IU CM and RNSSO SPL without using special equipment for each measurement step, simplifies control technology, reduces assembly time CM, takes into account effect of deformations of structure CM and SPL chassis on mutual position of IU CM and RNSSO SPL, reduces no-flight time of IU CM in inertial mode.
EFFECT: invention can be used for aiming cruise missiles.
1 cl, 4 dwg
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Authors
Dates
2020-01-13—Published
2019-07-16—Filed