FIELD: aircrafts.
SUBSTANCE: invention relates to a method for including a preformed maneuver into a flight mission of an unmanned gliding aircraft (UAV). To include the maneuver in the flight task, the conditional coordinates of the control points of the maneuver are transformed in a certain way. The obtained coordinates of the control points are included in the data of the flight mission of the UAV. To a given set of reference points of any maneuver in the conventional coordinate system, one more reference point is added in advance in the vertical coordinate plane at a distance from the point considered to be the first, sufficient to turn the UAV with maximum speed in the direction of the second reference point of the maneuver. The last reference point of the UAV trajectory sustainer is set at a distance from the target equal to the distance of the first UAV maneuver point from the origin of the conventional coordinate system.
EFFECT: improved UAV guidance accuracy.
1 cl, 3 dwg, 2 tbl
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR FORMATION OF MANOEUVRES OF ARBITRARY CONFIGURATION ON TERMINAL TRAJECTORY OF UNMANNED GLIDING AERIAL VEHICLE | 2013 |
|
RU2554568C2 |
CONTROL METHOD OF AN UNMANNED GLIDING AIRCRAFT ON TRAJECTORIES WITH CHANGES OF DIRECTIONS OF MOVEMENT IN THE SPECIFIED REFERENCE POINTS | 2019 |
|
RU2708412C1 |
METHOD OF CONTROLLING UNMANNED PLANNING AERIAL VEHICLE | 2017 |
|
RU2654238C1 |
METHOD FOR CORRECTING THE FORMED CONFIGURATION OF THE ROUTE OF AN UNMANNED GLIDING AIRCRAFT | 2020 |
|
RU2749990C1 |
METHOD OF REDUCING THE SPEED AND TIME LOSS IN IMPLEMENTATION OF MANEUVRE OF SPECIFIED CONFIGURATION BY UNMANNED AERIAL VEHICLE OF VOLPLANE TYPE | 2016 |
|
RU2623361C1 |
COMPLEX FOR DETERMINING THE SPATIAL COORDINATES OF A REMOTE OBJECT LOCATED ON THE GROUND | 2020 |
|
RU2744427C1 |
METHOD OF CONTROLLING GROUP OF MANEUVERABLE UNMANNED AERIAL VEHICLES | 2022 |
|
RU2818981C1 |
WINGED MISSILE AND METHOD OF ITS COMBAT UTILIZATION ( VARIANTS ) | 2002 |
|
RU2225975C1 |
MODE OF GIVING ASSIGNMENT FOR TRAFFIC ROUTE OF A GLIDING FLYING VEHICLE WITH TERMINAL CONTROL | 2003 |
|
RU2251664C1 |
TARGET DESTRUCTION METHOD BY VOLLEY OF ATMOSPHERIC AIRCRAFTS | 2016 |
|
RU2691233C2 |
Authors
Dates
2021-10-07—Published
2020-12-09—Filed