FIELD: physics, navigation.
SUBSTANCE: invention relates to avionics and devices for signalling proximity with the ground or high obstacles. The technical result is achieved due to that the obstacle sensor comprises a radio transmitter with a directional antenna which periodically emits radiation pulses based on a command from a multivibrator, a radio receiver, an electronic switch controlled by a timing relay, a second timing relay, an amplifier, a light and/or audio indicator; the sensor may include two or more such independent sensors; antenna sectors of which partially overlap in space; the sensor may include a multi-position "running lights" type circuit which cyclically connects the directional antenna to the corresponding LED.
EFFECT: reducing the dimensions of the antenna by selecting a high operating frequency and reducing transmitter power and receiver sensitivity.
7 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
STAROVEROV RADAR | 2009 |
|
RU2429502C2 |
ALTITUDE INDICATOR | 2010 |
|
RU2428657C1 |
ANTI-HELICOPTER AND ANTI-STEALTH MISSILE | 2009 |
|
RU2443968C2 |
EXTRA INDICATOR OF PITCH AND/OR VERTICAL SPEED (VERSIONS) | 2014 |
|
RU2567985C2 |
MAN-PORTABLE AIR DEFENSE SYSTEM AND ITS OPERATION METHOD | 2015 |
|
RU2593532C1 |
PARACHUTE SYSTEM/VERSIONS AND ITS CONTROL SYSTEM/VERSIONS | 2013 |
|
RU2561182C2 |
EMERGENCY LANDING SYSTEM | 2006 |
|
RU2335437C2 |
NON-CONTACT DETONATING FUSE (VERSIONS) | 2009 |
|
RU2412427C2 |
SYSTEM OF ANTI-MISSILE DEFENCE SUPPRESSION, ITS ALGORITHM AND WARHEAD | 2014 |
|
RU2611683C2 |
PORTABLE SURFACE-TO-AIR MISSILE SYSTEM /VERSIONS/ | 2012 |
|
RU2514324C1 |
Authors
Dates
2014-08-27—Published
2012-06-20—Filed