FIELD: aviation.
SUBSTANCE: invention relates to methods for automatic aircraft landing. For automatic landing in difficult weather conditions horizontal distance is set from initial point of trajectory decrease to its end point, parameters of aircraft movement in final point trajectory reduction, measuring speed and flight altitude, horizontal distance to final point of trajectory reducing deviation from vertical plane of axial line of runway, vertical component of flight speed, pitch, roll angles are determined and vertical component of aircraft velocity in a certain manner depending on difference of distances defined on propagation time of signals from transceivers lying in a certain manner through defined time interval, fed to missile control commands of aircraft in case of deviation value obtained by comparing next and previous calculation data along vertical component of velocity of aircraft.
EFFECT: safe landing in difficult weather conditions.
5 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2011 |
|
RU2478523C2 |
METHOD OF CONTROL OF AIRCRAFT ON THE APPROACH | 2004 |
|
RU2267747C1 |
TAKE-OFF AND LANDING DISPLAY SYSTEM OF THE AIRCRAFT | 2016 |
|
RU2647344C2 |
METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2012 |
|
RU2496131C1 |
METHOD FOR AUTOMATIC CONTROL OF LONGITUDINAL MOVEMENT OF AIRCRAFT ON LANDING | 2018 |
|
RU2708785C1 |
METHOD OF PERFORMING DESCENT AT LANDING APPROACH | 2002 |
|
RU2280888C2 |
AIRCRAFT LANDING SYSTEM WITH APPLICATION OF DIGITAL TECHNOLOGIES | 2020 |
|
RU2734173C1 |
METHOD OF AUTOMATIC DRONE LANDING FOR MONITORING OF LONG STRUCTURES | 2012 |
|
RU2503936C2 |
METHOD OF CONTROL OF AIRCRAFT LANDING PATH AT LANDING ON PROGRAMMED AIRFIELD | 2013 |
|
RU2549145C1 |
METHOD OF AIRCRAFT PATH CONTROL IN LANDING APPROACH | 2013 |
|
RU2549506C2 |
Authors
Dates
2016-05-27—Published
2015-06-02—Filed