FIELD: navigational complexes of multi- mission fighters. SUBSTANCE: navigational complex includes inertial navigational system, satellite navigational system, navigational computer, navigations information recorder, internal navigational system error computer, storage unit, computer of corrections to velocity and azimuthal angle components of gyroplatform of inertial navigational system. Output of inertial navigational system is connected with first input of navigational computer and first input of recorder. Output of satellite navigational system is connected with second input of computer and second input or recorder. Output of recorder is connected with input inertial system error computer whose output is connected with of storage unit. Output of storage unit is connected with third input of navigational computer and input of velocity and azimuthal angle component correction computer whose output is connected with fourth input of computer. EFFECT: enhanced accuracy, trouble-free operation and informative capacity. 1 dwg
Title | Year | Author | Number |
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|
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COMBINED NAVIGATIONAL COMPLEX OF FLYING VEHICLE | 2003 |
|
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FLYING VEHICLE NAVIGATION COMPLEX | 2005 |
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NAVIGATION AND ELECTRONIC DISPLAY COMPLEX | 2003 |
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|
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|
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INDICATION SYSTEM OF AIRCRAFT | 2001 |
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COMPLEX NAVIGATIONAL SYSTEM | 2000 |
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MULTIFUNCTIONAL ABOARD INDICATOR | 2000 |
|
RU2162204C1 |
Authors
Dates
2001-07-10—Published
2000-11-30—Filed