FIELD: systems for navigation and orientation of mobile objects. SUBSTANCE: device has four sensitive members each of which is designed as string which is connected to inertia weight. In addition device has units for excitation of string oscillations. Axes of strings are located at given angles with respect to measuring axes of acceleration meter. EFFECT: increased functional capabilities. 1 tbl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ACCELEROMETER | 1986 |
|
SU1840348A1 |
ACCELEROMETER | 1988 |
|
RU2046347C1 |
STRING ACCELEROMETER | 1969 |
|
SU1840379A1 |
ACCELEROMETER | 1989 |
|
RU2046348C1 |
STRING ACCELEROMETER | 1981 |
|
SU1840364A1 |
ACCELEROMETER | 1986 |
|
RU2085954C1 |
METHOD DETERMINING ORIENTATION OF OBJECTS IN SPACE, RANGE TO THEM AND BEARING, POSITION COORDINATES AND COMPONENTS OF VELOCITY VECTOR BY NAVIGATION RADIO SIGNALS OF SPACECRAFT OF SPACE RADIO NAVIGATION SYSTEMS | 1998 |
|
RU2152625C1 |
ACCELEROMETER | 1990 |
|
RU2018852C1 |
THREE-COMPONENT PIEZOELECTRIC ACCELEROMETER | 0 |
|
SU1760462A1 |
INERTIA SYSTEM OF ANGULAR ORIENTATION | 1977 |
|
SU1839897A1 |
Authors
Dates
1998-01-10—Published
1995-11-15—Filed