FIELD: transport.
SUBSTANCE: invention relates to aircraft landing control in emergency at failures of both onboard automatic radio compasses (ARC) and ground radio homing beacon (GRHB) to direct aircraft to landing start point (LSP). Proposed method consists in driving the aircraft to LSP with the help of radar irradiation warning station (RIW) and two sources of radio radiation (RIS) operated on separated frequencies covered by frequency range of RIW and mounted at GRHB and near homing beacons (NHM) to indicate runway lengthwise axis. Note here that RIW frequencies are preloaded into aircraft RIW bank while their spacing must make 500-1000 MHz. Depending upon relative position of aircraft and two ground RIW allow three versions of method implementation. Proposed landing processes allow driving the aircraft to LSP at failure of onboard radio communication means and automatic radio compasses and can be used for emergent landing of aircraft equipped with RIW.
EFFECT: higher flight safety.
3 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT LANDING APPROACH AND SYSTEM TO THIS END | 2014 |
|
RU2559196C1 |
| APPROACH METHOD OF UNMANNED AERIAL VEHICLE IN EMERGENCY CONDITIONS | 2019 |
|
RU2725640C1 |
| METHOD OF DETERMINING THE COORDINATES OF AN AIRCRAFT RELATIVE TO THE FLIGHT STRIP | 2016 |
|
RU2620587C1 |
| AIRCRAFT INSTRUMENT APPROACH SYSTEM BASED ON RADIO BEACONS INDICATING BEGINNING OF LANDING STRIP | 2012 |
|
RU2492525C1 |
| METHOD AND SYSTEM FOR CONTROL OF AIRCRAFT AT ENGINELESS LANDING | 2005 |
|
RU2321524C2 |
| METHOD AND DEVICE FOR CONTROLLING GLIDE PATH POSITION AND COORDINATES OF AIRCRAFT IN FAR ZONE | 2018 |
|
RU2692079C1 |
| METHOD FOR APPROACH LANDING | 2002 |
|
RU2242800C2 |
| METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2012 |
|
RU2496131C1 |
| FLYING VEHICLE AUTOMATIC LANDING SYSTEM | 2004 |
|
RU2284058C2 |
| METHOD OF AIRCRAFT PATH CONTROL IN LANDING APPROACH | 2013 |
|
RU2549506C2 |
