FIELD: military hardware.
SUBSTANCE: data are retrieved from the route navigation system of survey control and orientation (RNSSCO) from the self-propelled launcher (SPL) assembly and results of measurements of angular mismatches between axes of the inertial navigation system (INS) of the missile and RNSSCO. The angular route mismatches between a longitudinal axis of the missile INS and RNSSCO longitudinal axis and the subsequent use of results of the taken measurements during pre-starting procedure for determination of a true azimuthal angle of the missile by estimation of correction to the azimuthal angle measured by RNSSCO. The array of angular corrections measured by INS, missiles and SPL manufacturers is saved in permanent memory units.
EFFECT: higher accuracy.
3 dwg, 1 tbl
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|---|---|---|---|
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| METHOD OF AIMING CRUISE MISSILES IN VERTICAL LAUNCHERS | 2018 |
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RU2285889C1 |
| METHOD FOR PRE-LAUNCH SETTING OF HIGH- ACCURACY MISSILES | 1995 |
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RU2150124C1 |
| SELF-PROPELLED LAUNCHER | 2007 |
|
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| ROLLING CRUISE MISSILE | 2014 |
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| MOBILE ANTIAIRCRAFT GUIDED MISSILE SYSTEM | 2003 |
|
RU2253820C2 |
| CRUISE MISSILE AND METHOD OF COMBAT USE THEREOF | 2017 |
|
RU2713546C2 |
| GUIDANCE SYSTEM OF FAR-ZONE HIGH-ACCURACY WEAPON | 2003 |
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RU2284444C2 |
