FIELD: navigation. SUBSTANCE: proposed gyroscopic navigation system is intended for sea, air and land objects. System incorporates unit for control and generation of output parameters, gyroplatform with two-degree of freedom gyros and two accelerometers. System is additionally inserted with units of turn of sensitive elements and unit of vibrations of gyroplatform which provide for modulation of system errors on different frequencies. EFFECT: enhanced accuracy of system. 3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PROCESS GENERATING NAVIGATIONAL PARAMETERS AND ELEVATION VERTICAL | 1997 |
|
RU2126136C1 |
| PROCESS GENERATING NAVIGATIONAL PARAMETERS AND ELEVATION VERTICAL | 1998 |
|
RU2147731C1 |
| GYROPLATFORM STABILIZED IN HORIZON PLANE | 1993 |
|
RU2047093C1 |
| PROCESS OF GENERATION OF NAVIGATION PARAMETERS | 2001 |
|
RU2197716C2 |
| PROCESS GENERATING NAVIGATIONAL PARAMETERS AND POSITION VERTICAL | 1998 |
|
RU2138018C1 |
| GYROSCOPE NAVIGATION SYSTEM | 1998 |
|
RU2145058C1 |
| PROCESS OF GENERATION OF NAVIGATIONAL PARAMETERS AND ELEVATION VERTICAL | 1997 |
|
RU2120608C1 |
| METHOD OF DETERMINATION OF NAVIGATIONAL PARAMETERS AND LOCAL VERTICAL | 1991 |
|
RU2046289C1 |
| METHOD OF GENERATION OF NAVIGATIONAL PARAMETERS AND LOCAL VERTICAL | 2002 |
|
RU2206067C1 |
| METHOD OF MEASURING NAVIGATION PARAMETERS AND SITE VERTICAL | 2005 |
|
RU2309384C2 |
