FIELD: radio engineering. SUBSTANCE: airborne differential distance analyzer has receiving antenna 1, receiver 2, amplifier 2, range-marker generator 4, discriminators 5,8, adders 6,9,21,24,28, variable-frequency oscillators 11,13, phase changer 12,14, reference generator 15, searching unit 16, control unit 17, coding signal driving generator 18, gate-pulse driver 19, controlled delay timer 20, horizontal-flight velocity component-to-geographical coordinate converter 33, subtraction units 23, 27, 34, 35, 38, 39,41, low-pass filters 25,29,40, multipliers 26,30,31,32, divider 36 and functional generator 37. EFFECT: increased measurement accuracy. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
DISTANCE MEASURING COMBINED SYSTEM | 1992 |
|
RU2022297C1 |
GAS CURRENT AND DIRECTION METER | 1992 |
|
RU2041463C1 |
AIRBORNE COMPLEX SYSTEM MEASURING DISTANCE AND AZIMUTH | 0 |
|
SU1529951A1 |
METHOD FOR RUNNING FULL-SCALE TESTS OF RADIO ELECTRONIC SYSTEMS | 1997 |
|
RU2137193C1 |
DEVICE FOR PROTECTION OF INNER FLOW OF DOUBLE-FLOW TURBOJET ENGINE AGAINST FOREIGN MATTER | 1992 |
|
RU2045451C1 |
COMPLEX RADIO-NAVIGATIONAL SYSTEM FOR MEASURES AIRCRAFT AZIMUTH RELATIVELY RADIO BEACON | 0 |
|
SU1398607A1 |
SYSTEM FOR DETERMINING COURSE OF MOBILE OBJECT | 0 |
|
SU1385110A1 |
COMPLEX NAVIGATIONAL SYSTEM | 1992 |
|
RU2115890C1 |
AIRBORNE TWO-COORDINATE RADIO DIRECTION FINDER | 0 |
|
SU1484105A1 |
COMPLEX RANGE FINDER | 0 |
|
SU1396103A1 |
Authors
Dates
1994-08-30—Published
1991-05-12—Filed