FIELD: engineering of autonomous optical and radiolocation systems for preventing collisions of an aircraft with obstacles by warning the crew members about obstacle directions and distances towards them.
SUBSTANCE: the indicator consists of control system and light-emitting modules, which emit radiation in various sections of visible spectrum. Light-emitting modules with their control blocks are combined in "n" sectors based on number of collision prevention system observation channels, each one of which is divided on "m" illuminated zones along sector generating lines which have their own coloring which corresponds to certain range of distance to the obstacle. Sector opening angle equals the angle of prevention of corresponding collision prevention system channel and their combined placement matches the whole warning area in flight plane of the aircraft. When given indicator is present in collision prevention system, precise detection of azimuth and distance to the obstacle is not necessary, only detection of zone (sector) where the obstacle is located, and interval of distances between the aircraft and the obstacle.
EFFECT: possible application of collision prevention system during flight in complicated conditions.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RADAR SYSTEM WHICH ALARMS AIRCRAFT AGAINST COLLISION | 1999 |
|
RU2150752C1 |
| AIRCRAFT LANDING APPROACH AND SYSTEM TO THIS END | 2014 |
|
RU2559196C1 |
| FLYING VEHICLE COLLISION WARNING DEVICE | 1997 |
|
RU2131622C1 |
| SYSTEM AND METHOD FOR DETECTING OBSTACLES IN AIR TRAFFIC SYSTEMS | 2018 |
|
RU2762151C2 |
| SHORT-RANGE RADAR SYSTEM FOR COLLISION WARNING OF AIRCRAFT MANEUVERING ON AIR FIELD | 2001 |
|
RU2192653C1 |
| RADAR METHOD FOR PREVENTING COLLISION OF AIRCRAFT WITH OBSTACLES IN VERTICAL PLANE AND DEVICE FOR REALISING SAID METHOD | 2009 |
|
RU2428713C2 |
| METHOD OF CONTROLLING LOW-ALTITUDE FLIGHT OF AIRCRAFT IN VERTICAL PLANE | 2023 |
|
RU2822805C1 |
| DEVICE FOR PREVENTION OF HELICOPTER COLLISION WIT OBSTACLES | 2007 |
|
RU2370786C2 |
| METHOD OF DETERMINING THE COORDINATES OF AN AIRCRAFT RELATIVE TO THE FLIGHT STRIP | 2016 |
|
RU2620587C1 |
| COLLISION AVOIDANCE SYSTEM FOR FLIGHT TESTS | 1996 |
|
RU2134911C1 |
