FIELD: radio engineering, communication.
SUBSTANCE: result is achieved by reducing the size of antennae used, which considerably reduces the weight and overall dimensions of landing support systems compared to existing instrument landing systems.
EFFECT: improved weight and size characteristics of the system.
4 dwg
Title | Year | Author | Number |
---|---|---|---|
ERROR SIGNAL GENERATION AT CONTROL OVER OBJECT PLACING TO PRESET POINT | 2013 |
|
RU2556890C2 |
LOCAL PHASE DIFFERENCE-RANGE-FINDING RADIO NAVIGATION SYSTEM | 2015 |
|
RU2604652C2 |
METHOD OF DETERMINATION OF ORIENTATION OF OBJECT | 1992 |
|
RU2036826C1 |
RADIO NAVIGATION SYSTEM FOR MEASUREMENT OF MOBILE OBJECT BEARING | 2012 |
|
RU2507529C1 |
RADIO NAVIGATION SYSTEM FOR MEASUREMENT OF MOBILE OBJECT BEARING | 2012 |
|
RU2507530C1 |
METHOD FOR DETERMINING AIRCRAFT POSITION WITH RESPECT TO RUNWAY AT LANDING AND SYSTEM FOR ITS IMPLEMENTATION | 2016 |
|
RU2620359C9 |
QUERY-BASED METHOD OF MEASURING RADIAL VELOCITY AND POSITION OF GLONASS GLOBAL NAVIGATION SYSTEM SATELLITE AND SYSTEM FOR REALISING SAID METHOD | 2012 |
|
RU2518174C2 |
METHOD FOR RADAR LOCATION OF OBJECTS WITH INERTIAL NONLINEARITY | 2013 |
|
RU2510765C1 |
METHOD OF PREVENTING UNAUTHORISED USE OF AIRCRAFT | 2012 |
|
RU2509373C2 |
METHOD OF LOCATING NAVIGATION OBJECT | 2015 |
|
RU2584545C1 |
Authors
Dates
2015-02-27—Published
2013-10-17—Filed